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Longer titles found: Apollo Abort Guidance System (view), Stand guidance system (view), Flash flood guidance system (view), Electronic Route Guidance System (view)

searching for Guidance system 495 found (1950 total)

alternate case: guidance system

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display, or heads-up display, also known as a HUD (/hʌd/) or head-up guidance system (HGS), is any transparent display that presents data without requiring

missile, and calculates whether their paths will intersect. If not, the guidance system will relay commands to a missile, telling it to move the fins in a

version of the earlier Blowpipe of the 1970s. Blowpipe used a manual guidance system which proved hard to use effectively in combat during the Falklands

name RASCAL was the acronym for RAdar SCAnning Link, the missile's guidance system. The RASCAL project was cancelled in September 1958. During World War

munitions (PGMs). JDAM-equipped bombs are guided by an integrated inertial guidance system coupled to a Global Positioning System (GPS) receiver, giving them

flies, the wires are reeled out behind it (command guidance). This guidance system is most commonly used in anti-tank missiles, where its ability to be

favor of the newer FGM-148 Javelin system. The M47 Dragon uses a wire-guidance system in concert with a high explosive anti-tank warhead and was capable

November 1974, a cable connecting the pitch rate control gyroscope to the guidance system became disconnected, resulting in a loss of control and launch failure

based on the AGM-12C/E Bullpup missile, was fitted with an inertial guidance system, and had a radar altimeter-based fuse to ensure an airburst of the

Inversion therapy, or simply inversion, is the process of seeking therapeutic benefits from hanging by the legs, ankles, or feet in an inverted angle or

weight of the guidance system, and an increase in the survivability of the guidance system in a nuclear environment. The guidance system contained 2,000

fully internal inertial guidance system. Later Atlas E/F models were equipped with what would have been the Titan I's guidance system The Titan I would be

trajectory complications with lunar gravity. However, on re-entry the L1's guidance system failed. It hit the atmosphere precisely at the calculated time, but

Intelligent Parking Assist System (IPAS), also known as Advanced Parking Guidance System (APGS) for Toyota models in the United States, is the first production

on the Zolfaghar SRBM which some sources suggest does have a poor guidance system. In the words of Iranian defense minister Amir Hatami the missile is

hard to obtain, it was replaced by a more modern guidance system, the Delco Universal Space Guidance System (USGS). The USGS used a Carousel IV IMU and a

parlance, a rocket differs from a missile primarily by lacking an active guidance system; early missiles became known as "guided rockets" or "guided missiles"

obtain, it was replaced by a more modern guidance system, the Delco Electronics Universal Space Guidance System (USGS). The USGS used a Carousel IV IMU

and using a novel guidance system involving optical beam-riding, the program was unable to resolve difficulties with the guidance system and was cancelled

was an Israeli medical device company and manufacturer of a robotic guidance system for spine surgery that was acquired by Medtronic in December 2018.

aerial targets like helicopters. The 9M123 missile, and its associated guidance system, forms the 9K123 missile system. The Khrizantema anti-tank missile

and using a small joystick to adjust its flight. The original manual guidance system was replaced in 1967 to produce the Harpon version, which used SACLOS

leaking LOX started pushing the stage off its proper flight path. The guidance system tried to compensate by repeatedly firing the attitude control jets

the United States Army Air Forces during the late 1940s. Mating the guidance system of the earlier Razon radio-controlled weapon with a British Tallboy

proper mix of food groups in one's diet. As part of the MyPyramid food guidance system, consumers were asked to visit the MyPyramid website for personalized

portion of the Blok E stage remained attached to the payload and the guidance system was modified specially to assist in putting payloads in sun-synchronous

Semi-active radar homing (SARH) is a common type of missile guidance system, perhaps the most common type for longer-range air-to-air and surface-to-air

new motor, the FG-36 and an optional RCS. A new computer inertial guidance system which enabled the third stage to be 3-axis stabilised for added precision

was replaced by the near-identical Atlas I, which had an improved guidance system and offered a larger payload fairing. Atlas G was an evolution of the

AGM-65 Maverick which employed contrast lock technology, the -Kr series guidance system employs Scene Matching Area Correlation technology more akin to the

guided by two different systems; the ‘posterior’ guidance system and the ‘anterior’ guidance system Posterior guidance refers to TMJ articulations and

ground guidance aside from a few R&D launches which tested the inertial guidance system designed for the Atlas E/F, and the Atlas D would be the basis for

of the eight first-stage Saturn I engines shut down early, but the guidance system compensated by burning the remaining seven engines longer. AS-101 was

match the performance of the existing MX ICBM. Modifications to the guidance system, electronics hardening, and external protective coatings were incorporated

system was in competition with the IR-guided Gyurza system. The IR guidance system of the Gyurza missile proved troublesome and the Kobra was put into

contract, AC Spark Plug the primary inertial guidance system, Bell Labs the backup radio guidance system, and General Electric the nose cone/reentry vehicle

interface and airborne launch testing, and SM-K/I and SM-K/II for guidance system and ground launch testing. First SM-20/I launch from Tu-95K was made

missile. The missile, named the AGM-53A Condor, was to use a television guidance system with a data link to the launching aircraft similar to the system of

November 1958. After Pioneer 1 had failed due to guidance system deficiencies, the guidance system was modified with a Doppler command system to ensure

solid-fueled Thiokol TX-20 rocket, and was equipped with an advanced inertial guidance system derived from that of the AGM-28 Hound Dog cruise missile. Four tailfins

older analog guidance system with a solid state version that could operate with the F-15's new pulse-doppler radar. The guidance system was much smaller

development started in the late 1940s, emerging in the early 1950s as a guidance system for the modular Zuni rocket. This modularity allowed for the introduction

RUR-5 ASROC with an upgraded solid-fuel booster section and a digital guidance system. It carries a lightweight Mark 46 homing torpedo that is dropped from

design had a range of 350 km, which was later increased to 450 km. The guidance system was an inertial platform which could be programmed to execute evasive

equipped with a 650 kg explosive warhead and an interception evading guidance system. The missile was unveiled in February 2011 when the Commander of the

equipped with the GAM-83A. For training purposes, Martin produced a guidance system that could be fit to surplus High Velocity Aircraft Rockets, which

F112-WR-100 turbofan engine increased range by about 50%. The newer guidance system increased accuracy to a quoted figure of between 30 m (100 ft) and

coordinated system. One such project is the introduction of the Parking Guidance System (PGS) in the city and HarbourFront area to guide drivers to the nearest

missile is outside the atmosphere and on a sub-orbital trajectory. The guidance system for the missile was developed by the Charles Stark Draper Laboratory

unit. There was also an extensive forward guidance system composed of a radar, four Missile Guidance System units, and several other units including a

version of the earlier AS-20 design, and initially used that weapon's guidance system, which required pilots to track the weapon visually and correct its

Recent studies indicate movement along the processes of FDC as a guidance system for mature resting B cells in peripheral lymph nodes. Unlike their

to take up the development of a replacement for Malkara using a new guidance system developed in-house. Malkara was one of the earliest anti-tank missiles

its target, combined with a precise and high-performance terminal guidance system with advanced sensors and in-flight calibrations in order to successfully

Gee, sometimes written GEE, was a radio-navigation system used by the Royal Air Force during World War II. It measured the time delay between two radio

multiple-launch, radar-guided missile: one which used its own active guidance system to guide itself without help from the launch aircraft when it closed

system. The Bullpup was manually steered onto the target, whereas the guidance system in the Blue Eye was an optical area correlation seeker. A TV camera

unguided rockets that it was intended to replace. Studies regarding the guidance system of the LFSW were conducted by the Applied Physics Laboratory, which

improved version of the RAM missile that adds an overall infrared-only guidance system that enables it to intercept missiles that are not emitting any radar

Iran's similar shaped Zelzal rockets, Naze'at rockets do not have a guidance system. Both systems are also widely known without the -H suffix, as the Naze'at

9.8 kilometers (6.1 mi). The weapon is not accurate as there is no guidance system, but it is extremely effective in saturation fire. BM-14 (8U32) - 16-round

terminal attack height of 7–10 m (23–33 ft); The missile has an inertial guidance system using GPS and BeiDou data, and an active terminal sensor. A 2017 China

initially designed to use the SHANICLE (Short Range Navigation Vehicle) guidance system. This was essentially an adaptation of the LORAN hyperbolic navigation

supersonic targets, and a flight altitude as low as 1.5 meters. The guidance system is said to be an advanced matrix imaging infrared (IIR) seeker. However

was expected to be stored in ready-to-fire form for months, and the guidance system used external fins for control instead of relying entirely on the steerable

India, and American bases in the Pacific. The missile uses an inertial guidance system, resulting in a large CEP of 1,500 meters. As of 2017, 10–15 launchers

greatly improved reliability. The reduction in volume from the new guidance system also enabled a larger warhead to be fitted, improving the missile's

Hydraulics (TsNIAAG) began work on the project in 1967, using an optical guidance system where a photograph of the target (provided through air reconnaissance)

Stagecoach Group signed a deal with Siemens to develop an optical guidance system for use in the United Kingdom. Two bus lines in Eindhoven, Netherlands

attached to the nose of the weapon and contains either a television guidance system for daytime or an imaging infrared system for night or limited, adverse

the powder-fuel accelerator. It also has a dual guidance system consisting of an inertial guidance system to guide it into the target area and a television

adoption of new radars and a continuous wave semi-active radar homing guidance system. It entered service with the US Army in 1959. In 1971 it underwent

weighed 1174 pounds (534 kg). The torpedo employed a passive acoustic guidance system and was intended for both submarine and surface targets. Nicknamed

booster engines resulted in below normal velocity, and consequently the guidance system did not generate the planned SECO (Second Engine Cut-Off) signal at

missile under the project name Kh-23, but they had problems developing a guidance system that would work with existing aircraft. As a result, Yurii N. Korolyov

fully instigated but not using the unsuitable Jupiter payload and guidance system. By October 1956, a study group comprising key figures from Navy, industry

M45 has a reported accuracy of 350 m CEP using an inertial missile guidance system coupled with computer payload control. It was succeeded by the M51

375,000 pounds-force (1,670 kN). Atlas E/F used the ARMA inertial guidance system rather than Atlas D's radio ground guidance; some IOC (Initial Operational

The GBU-57A/B MOP (Massive Ordnance Penetrator) is a precision-guided, 30,000-pound (14,000 kg) "bunker buster" bomb used by the United States Air Force

World War II, along with George Antheil, Lamarr co-invented a radio guidance system for Allied torpedoes that used spread spectrum and frequency hopping

Nimbus B never achieved orbit because a malfunction in the booster guidance system forced the destruction of the spacecraft and its payload during launch

rolling airframe missile system with infrared/radar dual mode hybrid guidance system. FB-10 missile is fitted on the Type 625/E self-propelled gun-missile

the I-RAAD has a different launcher with a tripod-mounted SACLOS guidance system that makes the missile much easier to aim. The specific SACLOS method

Taylor Model Basin was to assist with hydrodynamics and propulsion. The guidance system used four hydrophones on the torpedo's midsection, connected to a vacuum

1 was a test of the performance capabilities of the propulsion and guidance system of the booster and satellite. The launch took place from Vandenberg

cross-wiring with the engine that had shut down. The vehicle's onboard guidance system compensated by burning the second and third stages longer, although

"tramways on tyres", and in common with tram systems they use a surface guidance system and in normal operation are powered by electricity drawn from an overhead

contrast seekers, or simply contrast seekers, are a type of missile guidance system using a television camera as its primary input. The camera is initially

October 2010; the construction costs amounted to 340,000 euros. A guidance system is also available. J. Meyer-Kronthaler: Berlins U-Bahnhöfe. be.bra

system for production examples. Fairchild referred to the combined guidance system as "Skylark". During the early and mid-range stages of flight, existing

structure to support the added weight of upper stages, and the inertial guidance system replaced with a radio ground guidance package, which was moved to the

hundreds). The accident investigation identified a failure in the guidance system of the Long March 3B. After the Intelsat 708 accident, the Long March

platform pavement was replaced by natural stone slabs and a blind guidance system was installed. Rehberge station is located towards the northern end

warfare ability, to bring down low flying helicopters, due to its wire-guidance system. An agreement was reached in 1989 between the French and Canadian governments

image processing. He was part of the team that built the MADDIDA, guidance system for Northrop's Snark cruise missile – one of the first digital computers

earlier. This was the first Atlas with a functional guidance system (although open loop—the guidance system was included merely for evaluation purposes and

the turret holds 18 missiles. The automatic command to line-of-sight guidance system uses both radar and IRST to locate a target and to track it and the

Television guidance (TGM) is a type of missile guidance system using a television camera in the missile or glide bomb that sends its signal back to the

the Atlantic Ocean. The failure was caused by a short circuit in the guidance system, which lost power and reset, causing the vehicle to pitch over. This

powered by a liquid-fueled rocket. It was fitted with a television guidance system, the pilot of the launching aircraft controlling the missile via radio

000 m) Depth: > 1,200 ft (370 m) Speed: > 40 kn (74 km/h; 46 mph) Guidance System: Homing mode: Active or passive/active acoustic homing Launch/search

Plant: Stored Chemical Energy Propulsion System Propulsion: Pump Jet Guidance system: Active/passive acoustic homing Warhead: 100 lb (45 kg) high explosive

GPS–INS guidance system. Increasing accuracy to a claimed 3m CEP is possible by adding an imaging infrared or a semi-active laser seeker terminal guidance system

stock of American-made Stinger MANPADS, since the Type 91 has a better guidance system, which consist of both visible light and infrared system options. The

the Viking rocket. Also developed as part of MX-774 was the Azusa guidance system which was not used on the Hiroc missile but did contribute to the Atlas

inclusive of all five food groups identified in the USDA MyPlate food guidance system (grains, vegetables, fruits, milk and meat and beans). As a state government

display since the guidance system position output is often taken as the reference point, resulting in a moving map), the guidance system could use this method

Military Periscope Monocular Guided Missile Sight, firing station and guidance system. It also carried a separate Barr & Stroud thermal imaging sight and

campaign for the Centers for Disease Control, the USDA MyPyramid food guidance system, and the M&M's Global Color Vote. The firm was founded in Washington

Stratofortress and then flew the rest of the way at about Mach 2. The guidance system was used to guide the first Polaris submarines. The booster engine

hole, which provides airspeed information necessary for its unusual guidance system. There are two rocket engines on the aft end, and two small rocket

speed 675 mph (1,090 km/h) Guidance system passive multiple-frequency radar seeker, autopilot and a radio-command guidance system Launch platform Aircraft

chances of launch failures. The inertial guidance system was replaced by a lighter-weight ground-radio guidance system The avionics truss in the second stage

first seen at Iran's 2010 Kish Air Show. As of 2016, the Sadid-1's guidance system, laser/TV seeker and propulsion unit were still under development.

submarine torpedo tubes. Chinese media claims the missile has an inertial guidance system using BeiDou Navigation Satellite System data, and carries a 300 kg

(bicycles, motorcycles, and ships) or be used as part of an inertial guidance system. MEMS gyroscopes are popular in some consumer electronics, such as

per 9P129 vehicle and raised prior to launch. It uses an inertial guidance system. The OTR-21 forward deployment to East Germany began in 1981,[citation

had a lethal radius of about 8 m (26 ft). It was thought that the guidance system would allow the pilot to get the missile into this range in terms of

engage any target from a mix of platforms using a reliable laser beam guidance system that was simple to use. It is a heavy ATGM, superior to the earlier

guided through a combination of an inertial guidance system plus a terrain contour-matching guidance system which uses radar and images stored in the memory

engine, which offered high speeds. The missile would use an inertial guidance system with terminal guidance provided by active radar homing—a mode of flight

where the rocket would ignite and its fins would deploy. An inertial guidance system would direct the missile to the general location of the target. Initial

any platform that had FLIR support, with the self-contained command guidance system able to be carried externally, or potentially integrated into existing

on a truck, ship or ground. Missile guidance is by GPS or Inertial guidance system for pinpoint accuracy at ranges of up to 50 km (31 mi). An optional

plus a forward-looking infrared (FLIR) set and a laser guidance system. The laser guidance system now made it possible to carry four 500-lb "smart bombs"

air-droppable unguided bombs into precision-guided bombs. The featured guidance system is a derivative of the respective system used in the "Popeye" (AGM-142

Attitude control was provided by hydrazine thrusters. The inertial guidance system used a ring laser gyroscope produced by Honeywell. Its control system

Shrike, which suffered from a small warhead, limited range and a poor guidance system. General Dynamics was asked to create an air-launched ARM by modifying

difference enables the guidance system of SY-300 to be rapidly changed in the field by soldiers, by simply replacing the guidance system with a dummy weight

payload. The guidance system was designed to provide navigation accuracies with an error of no more than half a percent. The guidance system proved to be

warhead, smaller than the 1.5 kiloton model used on the Genie. The guidance system allowed the missile to be used against maneuvering targets, including

vehicle was on the launch pad to provide gyroscopic force in lieu of a guidance system that would have required thrust vectoring, vernier thrusters, or a

personnel concentrations, and guerrillas. Nimrod has a semi-active laser guidance system that operates day or night. Its flight trajectory can be set below

control surfaces. This was assigned the code name "Red Rapier". For the guidance system, the Telecommunications Research Establishment (TRE) proposed an updated

Infrared homing is a passive weapon guidance system which uses the infrared (IR) light emission from a target to track and follow it seamlessly. Missiles

capable of striking targets at stand-off range. It has a terminal guidance system based on an infra-red imaging seeker which identifies the target during

theatrical feature documentaries, PGS - Intuition is your Personal Guidance System and Facing Fear are the first two films in a proposed series called

were allegations that aspects of Capricornio's design, such as its guidance system, had been derived from Condor missile developed by Argentina during

could be adapted to the role simply by replacing the original wire guidance system with a radio command link, and that its small size allowed multi-round

long enough to point directly back to the launcher. Additionally, the guidance system was difficult to use and had limited performance against moving targets

a German-produced anti-ship missile. The Kormoran uses an inertial guidance system for the midcourse phase, switching to active radar homing during the

Precision approach radar or PAR is a type of radar guidance system designed to provide lateral and vertical guidance to an aircraft pilot for landing

of Centaur's cryogenic fuels. The Centaur stage also contained the guidance system for the entire launch vehicle. A four-stage configuration was available

responsive to changes in trajectory. Iranian sources cite an improved guidance system on the missile, and analysts note that adjusting the missile's in-flight

April 1920, the remaining NiD-30s were fitted with an early audible guidance system. However, after a number of further accidents, these were withdrawn

A guidance system failure was suspected as the culprit, but JPL navigation chief Bill O'Neil dismissed the idea that the entire guidance system had

tail fin surfaces to prevent roll and so enhance the operation of the guidance system. The missile has a maximum effective range of 35 km [citation needed]

missile's trajectory is guided using small thrusters and an inertial guidance system on the warhead. The warhead is only a tenth of the size of the missile

capable of striking targets at stand-off range. It has a terminal guidance system based on an infrared homing seeker, which identifies the target during

accuracy MaRVs. In this case, it is the short range of the active guidance system that demands the RV be able to maneuver, as is the base in the Pershing

Positioning System (GPS) guidance system. The two other variants respectively integrate, in addition to the hybrid INS/GPS guidance system, either an infrared

by the United States during World War II. GB-4s used a television guidance system with the weapon being steered by a TV bombardier operating a joystick

are permitted, DME transponders are usually paired with an azimuth guidance system to provide aircraft with a two-dimensional navigation capability. A

seeker. The group managed to convince MIT of the need for a narrow beam guidance system and called the result "Mopsy". However, the US Navy lost interest in

columns. In 1941, Antheil and the actress Hedy Lamarr developed a radio guidance system for Allied torpedoes that used a code (stored on a punched paper tape)

anti-aircraft guns. The system is unusual as it uses a manual optical guidance system, sending guidance commands to the missile in flight over a radio link

that were of no concern for Mercury as it used a different model of guidance system and Atlas 6F and Samos 5 had random quality defects unlikely to be

Parking guidance and information (PGI) systems, or car park guidance systems, present drivers with dynamic information on parking within controlled areas

including helicopters, armored vehicles, small ships and infantry. The guidance system is based on video/infrared technology, with the missile connected to

was engineered by retrofitting the MU90 torpedo, particularly its guidance system. The power source was re-engineered to use a silver oxide battery.

Navy one year later. These missiles were designed around a television guidance system using a camera in the nose of the missile that sent its image back

no longer reliant on Russian components for missile production. The guidance system comprises data-linked mid-course guidance and active radar homing for

slightly heavier warhead (increased from 2.6 kg to 3 kg), a more accurate guidance system to increase the probability of a hit, and extended range. Range is

Mercury-Redstone's electronics and instrumentation, including the guidance system, as well as the adapter for the Mercury capsule. In the military Redstone

control devices, Honeywell Primus Epic avionics, standard head-up guidance system by Rockwell Collins and enhanced vision system by Elbit, improving

quickly narrowed the cause of the failure to a fault somewhere in the guidance system, but the exact nature of it could not be determined. It appeared that

have recovered an ATACMS missile guidance system intact, and stated that Russian officials are studying the guidance system to "identify any weak spots".

mass production in 2010. The Qaem anti-aircraft missile uses a laser guidance system. Iran also produces a variant, the Qaem-M, which adds a proximity fuse

control fins and two contra-rotating propellers. The vacuum tube-based guidance system is more sophisticated than earlier torpedoes, using pre-launch settings

final evolution of the Hatf I missile system. It includes an inertial guidance system that considerably improves the accuracy of the missile and is otherwise

2000 and Mamba missile systems, which were upgrades that improved the guidance system and performance of the missile. The missile had limited distribution

both missiles being designed by the same design bureau. The 9S816 guidance system is powered by a thermal battery attached to the launch tube shortly

Block IV: 100–200 nmi (190–370 km) Flight ceiling 80,200 ft (24,400 m) Maximum speed Mach 3.5 Guidance system Inertial/SARH Launch platform Surface ship

microwave landing system (MLS) is an all-weather, precision radio guidance system intended to be installed at large airports to assist aircraft in landing

Steel" which it would keep in service. With Elliots working on the guidance system, Armstrong Siddeley would develop the liquid fuel engine. The design

development. A key role was as an anti-shipping missile, using its guidance system to attack the moving targets. It would also replace unguided bombs

chassis, transporting up to 24 missiles. Versions with and without a guidance system for the missiles have been shown in designer drawings. Moreover, a

effects. On January 27, Missile 4C experienced a complete Mod III GE guidance system failure at T+80 seconds. The propellant utilization system operated

simulated riverboat cruise that travels along a waterway using a concealed guidance system through areas with Asian, African, and South American themes. Park

service on the M1 service using the guidance system, and London Buses later admitted in 2000 that the guidance system was not yet ready for deployment on

used as part of bus rapid transit schemes, and can include mechanical guidance system and electric bus or trolleybus. Articulated buses are typically 18 m

second stage were retracted prior to the spin up of the MHV. The MHV guidance system solely tracked targets in the field of view of the infrared sensor

Tor-M1, and operates at an altitude of 10 m to 10 km. The missile guidance system comprises semi-active radar homing by either the tracking radar, the

Another advantage in antitank applications is that the backward-looking guidance system does not interfere with the process of jet formation of high-explosive

homing ("heat seeking") missiles by confusing the missiles' infrared guidance system so that they miss their target (electronic countermeasure). Heat-seeking

probability of kill under most conditions. It has a semi-active laser guidance system, capable of both direct and indirect laser designation—the target can

Guidance Kit (PGK), formerly XM1156, is a U.S. Army-designed precision guidance system to turn existing 155 mm artillery shells into smart weapons. The prime

Vulcano module, which acts twofold: Programmer for ammunition's fuse and guidance system. Mission Planning and Execution for Naval Fire Support Action (firing

the Atlas guidance system had malfunctioned in flight, due to either a failure of the rate beacon or waveguide antenna, but the guidance system was not

first operational naval use in 2022. The land-attack variant has a new guidance system and was first fielded and used in 2023. "Long Neptune", an extended

prime contract in May, and in turn subcontracted to Northrop for the guidance system, Aerojet for the propulsion system, and General Electric for the reentry

Industries, aiming to exceed the performance of the original AIM-4D. The guidance system used infrared homing like the AIM-4D, but improved to a limited all-aspect

media reported that it has a range of 150 km, a speed of Mach 5, and a guidance system that enables it to hit a target independently of the launch aircraft's

aperture when compared to other optical devices being used by a typical guidance system for precision-guided munitions. Because of this, it is possible to

Immediately after liftoff, a short circuit of the launch vehicle's guidance system caused the Rocketdyne S-3D engines to gimbal, tilting the rocket sharply

SCAD in most ways, flew for the first time in March 1976, and its new guidance system was first tested that September. In January 1977, the missile was ordered

easier to use SACLOSTooltip semi-automatic command to line of sight guidance system (though only available for ground vehicle and helicopter mounts), as

0 mi) (slant, fast target) 15 kilometres (9.3 mi) (slant, slow target) Guidance system Command-guided version. Infrared homing Launch platform Transporter

Key to Cape Sable where he intends to steal the computerized missile guidance system and destroy the base to prevent discovery of the theft. At Cape Sable

robotic arm, along with an integrated image guidance system. During treatment, the image guidance system captures 3D images, tracks the movement of tumors

openings in the missile's metal parts and reaches its computers and guidance system. This energy is powerful enough to damage electrical components and

stages included the Centaur and Inertial Upper Stage. Guidance System: A ring laser gyro guidance system manufactured by Honeywell. Thrust: Stage 0: Solid

Designer Lockheed Missiles and Space Company Designed 1964 Specifications Warhead Cameras Engine Rocket Propellant Solid fuel Guidance system Ballistic

guidance system uses a combination of inertial navigation systems (INS), terrain contour matching (TERCOM) and GPS satellite guidance. The guidance system

taxiway system lit for night operations. It has a partial electronic guidance system consisting of a Localizer, Distance Measuring Equipment and a Non-directional

(110 kg) Engine Lockheed XSR13-LP-1 Propellant Solid fuel Maximum speed Mach 4 Guidance system Passive radar homing Launch platform F-4D, A-6B, F-105F

anti-aircraft missile that was the first to use a radio controlled guidance system. During the missile's development in the late stages of the war it

'anti-radar'). The main difficulty came in the design of the APR-28 guidance system undertaken by CKB-111 (later NPO Avtomatika). This meant that the Kh-28

mother worked on the Minuteman nuclear missile guidance system, the Apollo lunar module guidance system and the science ground station for the Hubble Space

its guidance system and a warhead with a greater range, a few small changes on the missile body, and a new re-entry vehicle whose terminal guidance system

integration onto Littoral Combat Ships. The Sea Griffin has a new motor and guidance system to increase its firing range from an LCS. Raytheon faced competition

low-level attacks. The Wagtail missile was intended to be fitted with a guidance system that utilised an inertial navigation system and a terrain-following

two of which were jettisoned during flight, a more sophisticated guidance system, and inflated balloon tanks that required constant pressure to not

included two vernier thrusters and the core stage included four. The guidance system was inertial with radio control of the vernier thrusters. The widely

homing, features a phased array active sonar and an improved wire guidance system: previous Soviet torpedoes had the guidance wire spool in the torpedo

Depth: 1,000 feet (300 m) Speed: 17 knots (31 km/h), 26 knots (48 km/h) Guidance system: active/passive sonar homing; passive until about 700 yards (640 m)

homing, features a phased array active sonar and an improved wire guidance system: previous Soviet torpedoes had the guidance wire spool in the torpedo

Operational range 2,500 km (1,600 mi) Maximum speed Around 185 km/h (115 mph) Guidance system AI pilot, GNSS, INS Launch platform Rocket-assisted take-off

The Mir cosmonauts did not feel the impact, though the station's guidance system registered angular velocity and switched to free flying mode. Later

Engine Solid-fuel rocket Operational range 4,600 miles (7,400 km) Guidance system Astro-inertial guidance Accuracy CEP: 229-500 m Launch platform Ballistic

Faced with Rafael Advanced Defense Systems's anxiety to develop a new guidance system, Shlomo Erell asked Israel Aerospace Industries to take over the program

Corporation between 1946 and 1949 to be used as a guidance system for the Snark missile. No guidance system, however, resulted from the work on the MADDIDA

760 lb), which includes the mass of a nuclear warhead and a terminal guidance system. Much of its engineering data, that is acceptable for public release

inertial guidance system, and a 1000CAP1 cluster warhead. Length: 8 metres (26 ft) Maximum diameter: 70 centimetres (28 in) Stages: 1 Fuel: HTPB Guidance system:

typically reads its position and the aircraft's attitude from an inertial guidance system. Inertial guidance systems accumulate errors over time. They will incorporate

package for that country's navy. P-20: A P-15 updated with the new guidance system but with the original shorter range. They were perhaps known as SS-N-2B

possible maximum range for that variant.[page needed] An inertial guidance system pilots the missile towards the target; for terminal homing the pilot

non-profit, volunteer organization Matador Automatic Radar Control, a guidance system for the Martin MGM-1 Matador cruise missile Mid-America Regional Council

single-chamber engine and uses a staged combustion cycle. The first-stage guidance system was open-loop, which required significant amounts of propellant to

fitted with stabilizing fins and a small course-correction rocket; the guidance system involved a radio command being sent to trigger the deflection charge

an orbital launch, Conestoga 1620, failed to achieve orbit due to a guidance system failure 46 seconds into its flight. The parent company, EER Systems

2004. Production was delayed for a year after a program error in the guidance system resulted in 2 failed tests in 2003. This glitch was fixed while developing

with a thrust-to-weight ratio goal of (4.6:1) to (5:1). The GAM-72s guidance system could be pre-programmed on the ground to execute two turns and one

DF-5A, with range increased to over 15,000 km and a more accurate guidance system. The DF-5A upgrade increased the throw-weight of the system from 7

largely useless on the battlefield. A new design emerged, combining the guidance system of the small Vickers Vigilant with a new and highly maneuverable missile

missile via a thin wire that trails behind the missile. The SACLOS guidance system has many benefits over manual command to line of sight (MCLOS), with

Production history Manufacturer  North Korea Specifications Mass 33.4 tons Length 25.8 m Diameter 1.8 m Engine liquid-fueled Guidance system inertial

of these rockets used liquid propellant. The A4b used an inertial guidance system, while the A9 would have been controlled by a pilot. They started from

States Navy Production history Designed 1973 Specifications Warhead PBX-W107 Guidance system Midcouse: semi-active radar homing Terminal: infrared homing

John Wong and Jeffrey Siewerdsen, of on-line volumetric kv-imaging guidance system for radiation therapy.[citation needed] He was named as one of "Canada's

torpedo 83R/URPK-3 Metel - Cruiser version of the missile using the guidance system from the SA-N-3 missile and the KT-106 launcher. Uses AT-1 torpedo

was delayed for several years because of issues with the IIR-based guidance system. The Nag missile underwent successful tests in September 1997 and January

however the RV impacted close to the target point. In addition, the guidance system rate beacon experienced difficulties early in the flight, however discreet

replaced by a new version, named Soyuz 2, which has a new digital guidance system and a highly modified third stage with a new engine. The first development

5. Range has been estimated at 400 km, 500 km, and 550–625 km. The guidance system is mixed-mode, with inertial guidance, terminal active radar homing

Couleur. MISTRAM was used in the development and testing of inertial guidance system for the Minuteman ballistic missile, and subsequently was used for

Mk 78 dual-thrust solid-fueled rocket Operational range 25 km (15.5 statute miles) Maximum speed 1,100 km/h (680 mph) Guidance system laser-guidance

original anti-shipping version and the air-to-surface version is in the guidance system. The original radar or IR-UV guidance of the C-704 is replaced a dual

(99 mi) (HQ-16C and HQ-16FE) Flight altitude 15m to 27km (HQ-16FE) Guidance system Semi-active radar homing Launch platform Transporter erector launcher

single-stage solid propellant motor with four exhaust nozzles. The guidance system had a TsNIIAG inertial platform with an onboard digital computer, coupled

Dan (6 February 2015). "US army seeks upgrades for Hellfire missile guidance system". Flight Global. Archived from the original on 30 March 2023. Raytheon

Oboe coupled radar tracking with radio transponder technology. The guidance system used two well-separated radar stations to track the aircraft. Two circles

high-G manoeuvres.[citation needed] The Block 3 missile accepts GPS guidance system waypoint commands, which allow it to attack naval targets from different

antenna or transmitter with minimal aircrew input. The proportional guidance system that homes in on enemy radar emissions has a fixed antenna and seeker

in 1969 when Bofors AB was contracted, who decided to use a novel guidance system in the form of a laser-beam riding missile co-developed with Laser

electronics, including the autoflight subsystem (e.g. flight management and guidance system). The air data module is a gas pressure sensor which converts mechanical

The tail kit is in a similar configuration to the Paveway I. The guidance system is unstabilized in roll, relying on bang–bang control like the Pavewave

energy weapons is that they require extremely high accuracy in the guidance system, on the order of 0.5 metres (2 ft). Exoatmospheric Kill Vehicle – Interceptor

transmission, including such as those from AWACS or UAV. The electro-optical guidance system provides a self-homing capability. The missile's on-board computer

200 nautical miles (5,900 km) Maximum speed 8,000 mph (13,000 km/h) (terminal phase) Guidance system Inertial Accuracy 0.3 nautical miles (560 m) CEP

of "maglev" in a United States patent was in "Magnetic levitation guidance system" by Canadian Patents and Development Limited. In 1912 French-American

missiles Engine integral rocket motor/ramjet booster and sustainer motor Guidance system command guidance with terminal semi-active radar homing (SARH)

impromptu meeting between the contractors led to a proposal to use the guidance system and ramjets to upgrade the Bloodhound Mk. I missile design. This private

additional weight as well as slightly reduced engine performance. The ARMA guidance system on 27E also experienced erratic behavior due to an intermittently shorted

The second stage housed the vehicle's telemetry system, the inertial guidance system and the autopilot. The third stage was spin-stabilized, with the spin

Laboratory's project to develop the Apollo Mission's navigation and guidance system. In 1968 Nordtvedt calculated how and to what degree the gravitational-to-inertial

Atlas soon vanished into an overcast gray sky. A malfunction of the guidance system rate beacon at T+93 seconds resulted in noisy track rate data, but

Autonomous underwater vehicle – Uncrewed underwater vehicle with autonomous guidance system Cryobot – Autonomous ice penetrator vehicle DEPTHX – Autonomous underwater

missile guidance, with commands transmitted over a wire link. The guidance system is constructed so that the most sophisticated and costly components

cruise to the target area, where they would use a secondary home-on-jam guidance system for terminal homing. During 1960, a Douglas A3D Skywarrior medium bomber

capable of reaching supersonic speeds. It is controlled by an inertial guidance system and uses thrust vectoring. Its maximum range is said to be over 30

MIRV Propellant Solid-fuel rocket Operational range >5,400 nmi (10,000 km) Guidance system Astro-inertial with Beidou Launch platform Type 094 submarine

laser-guided bombs were developed by Matra (now MBDA) starting in 1978. The guidance system had to work using the same principles as the US Paveway guided bombs

to 50 kilometres (27 nmi) and are guided by an integrated inertial guidance system coupled to three satellites networks, relying on wireless to handle

target, the LRASM is equipped with a BAE Systems-designed seeker and guidance system, integrating jam-resistant GPS/INS, an imaging infrared (IIR infrared

Williams F122-WR-100 turbofan Operational range 100 nmi (120 mi; 190 km)+ Guidance system INS With GPS updates Infrared terminal guidance Launch platform Proposed

Minuteman I ICBMs. The guidance system was based on technology developed during the earlier Homing Overlay Experiment. The guidance system used detected the

Between 1969 and 1975 he worked as a mathematical analyst for Aerospace Guidance System Center, Newark, Ohio. Since then until 1990 he worked as a research

rocket booster Operational range 55 km (34 mi) Maximum speed subsonic Guidance system Inertial guidance ballistic trajectory Launch platform Submarine

Qased Type Smart bomb Place of origin Iran Specifications Mass 2,000 lb (910 kg) Guidance system Unknown References

pounds (16 kg) Operational range 5 kilometres (3.1 mi) (maximum) Flight ceiling 2.5 miles (4.0 km) Guidance system Infrared homing Launch platform MANPADS

ASTOR had a range of approximately 5.5 to 7.5 nautical miles. The wire guidance system of the weapon was derived from the one developed for the Mark 39, alongside

vehicle prior to launch. The launch vehicle will have a target, and the guidance system will alter the steering commands to attempt to get to the final end

remotely, at a distance of up to fifty meters from the tripod mounted guidance system. It can be mounted on a Mitsubishi Type 73 jeep, similar to the Type

Vehicle possess antenna and other relevant parts of computerized guidance system needed to launch guided missiles, has new digital radio and Inertial

production being projected for the early 1950s; however its command-guidance system limited it to clear-weather, daytime use only. Although radar beam

mechanism Proximity fuse Propellant solid rocket fuel Operational range 40km Maximum speed 2.5 Mach Guidance system Infrared homing Launch platform Aircraft

objective was to test the performance of a Scout launch vehicle and its guidance system and to investigate the nature and effects of space flight on micrometeoroids

Proximity fused high-explosive Range: 93 km Fuse: Laser Proximity Guidance system: Pre-programmed/passive radar seeker Unit Cost: undisclosed Date Deployed:

forward-looking infrared (FLIR) and use a simple strapdown inertial guidance system to know where to look after launch. Examples of LOAL weapons include

altitude are identical. This produces a location and direction. The guidance system can then use this information to correct the flight path of the missile

Specifications Mass 500 kg Length 5 m Diameter 40 cm Propellant Solid fuel Operational range 90 km Maximum speed mach 4-5 Guidance system guided semi-active radar

guidance, the Kh-23, was first tested in 1968 but problems with the guidance system meant that it would not enter service for another five years. So in

(cruise), 5-10 m (attack) Maximum speed Mach 2.5-3.5, 2,716–4,321 km/h Guidance system Inertial navigation system (INS)/Satellite guidance Terminal radar/infrared

electro-optical guidance system. The anti-ship variant was dropped for budgetary and technical reasons, as the electro-optical guidance system and joystick

After the "Mackle" project was cancelled in 1956 the complex wire guidance system was transferred to the "Grog" program. This would be simplified, improved

Length 140 in (3.56 m) Diameter 13 in (340 mm) Maximum speed 700 m/s Guidance system unguided / laser-guided (S-25L) Launch platform Su-25, Su-25T, Su-25TM

bomb designed in 1939. The Schwartz design did not have a terminal guidance system; instead, it used an autopilot to maintain a straight course. It was

Engine Rocket engine Operational range 25 km Maximum speed Subsonic Guidance system Active radar or electro-optical Launch platform Ground, ship, air

by physical switches and recognized by appropriate logic. The sonar guidance system was developed for Mod I and improved for Mod II. It used two ultrasonic

system uses a semi-automatic command to line of sight (SACLOS) command guidance system. It tracks the missile either by a tail-mounted infrared lamp or an

300 miles (480 km) Maximum speed Mach 4.5+, test-flown to Mach 5.5 Guidance system Inertial + passive antiradiation and active radar homing for air-to-air

LBP-1 was fully capable of being remotely piloted via its TV-and-radio guidance system, it retained a cockpit, allowing the aircraft to be flown by a pilot

launcher, the provision of a missile handling room and a suitable guidance system. Seacat was used by NATO and Commonwealth navies that purchased British

maneuverable reentry vehicle (MARV) equipped with a radar terminal guidance system, which allowed it to use the lower-yield W85 warhead. This warhead

control devices for guided missile development; in 1950, an active radar guidance system was trialled using a CTV-N-2, successfully homing from a distance of

was featured in the film The Night My Number Came Up. An Instrument Guidance System (IGS) was installed in 1974 to aid landing on runway 13. Use of the

missile. The vibrations of the frame and fuel also interfered with the guidance system. The experience gained from solving these problems was applied not

had four stabilizing fins, and the vehicle incorporated a gyro-based guidance system for attitude stabilization to keep the rocket on course. San Marco

by physical switches and recognized by appropriate logic. The sonar guidance system was developed for Mod I and improved for Mod II. It used two ultrasonic

Makeyev Rocket Design Bureau Specifications Mass 32,800 kg (72,300 lb) Length 13.2 m (43 ft) Diameter 1.8m Propellant liquid Guidance system astro-inertial

(90 km) Flight ceiling 80,000 feet (24,000 m) Maximum speed >Mach 3 Guidance system Semi-active radar homing (SARH) with terminal infrared homing Launch

flying on NASA's Aqua satellite Advanced Inertial Reference Sphere, a guidance system designed for use in the LGM-118A Peacekeeper ICBM Put on airs, a phrase

The mission did complete the experimental testing of its stellar-guidance system and the ground-control of its radio telemetry equipment, its flight

which is fundamental to the operation of a gyrocompass or inertial guidance system that will be operated near the surface of the Earth. Schuler's cousin

Hitavada. 21 May 2021. Retrieved 12 September 2022. "WCR installs coach guidance system at 33 railway stations". The Hitavada. 28 July 2021. Retrieved 12 September

16 Gorgon IIIBs and 20 Gorgon IIICs also on contract. However, the guidance system had proved to be unworkable in tests of the Gorgon IIA missile, and

250–300 millimetres (9.8–11.8 in) (estimated) Operational range 300 km Guidance system Active radar with AESA Launch platform Chengdu J-20 Shenyang J-16

Mars Type Artillery rocket system Place of origin Soviet Union Specifications Maximum firing range 18 km (11 mi) Engine 3R1 Guidance system ballistic

reducing drag. Early designs may have relied solely on an inertial guidance system. The initial design was intended for nuclear warhead delivery. Later

by severe pogo oscillations. Starting with Apollo 10, the vehicle's guidance system was designed to shut the engine down in response to chamber pressure

Aircraft guidance system

control stations to maintain near-continuous contact with the craft. The guidance system, however, malfunctioned on the return leg, and the spacecraft performed

and storage space. The A3 plans called for a rocket with an inertial guidance system and a 1,500 kg (3,300 lb) thrust engine. In March 1936, Generaloberst

envisaged as a weapon against convoy escorts but with no effective guidance system, the arrangement was ineffective against moving targets and could only

Mk. II has the same range (70+ km), but the mid-course and terminal guidance system, as well as the radar and IR signature were upgraded. The Mk. II has

exhaust; the aircraft retained the Chukar's recovery parachute and radio guidance system, with the addition of a radar altimeter and midcourse guidance unit

its main axis due to a problem in a flotation gyroscope in the I-100 guidance system unit. A subsequent attempt to fire the main engine failed because of

Engine single-stage solid rocket motor Operational range 300-500 km Guidance system Inertial & electro-optical terminal Launch platform mobile launcher

optical fibre connects the flying missile's infrared camera and its guidance system. It can also be fired vertically and the fibre-optic cable is paid

Two-stage solid-fuel rocket 440 kN (99,000 lbf) Operational range 3,000 km (1,900 mi) Guidance system Inertial Launch platform Redoutable-class SNLEs (SSBNs)

shortages and deteriorated condition. Most notable was the inertial guidance system and mix computer. After the termination of V-2 flights by Hermes there

mechanism Contact fuze Engine Rocket engine Propellant Solid fuel Guidance system Laser beam riding, or millimeter wave radar Launch platform Tripod

the Agni-V to its target. However, Agni-V is equipped with another guidance system called micro inertial navigation system (MINGS) as a backup. These

retrorockets ignite to cushion the landing. A malfunction in the booster guidance system resulted in excessive spacecraft speed. Reversed command signals caused

solid-fuel rocket Operational range 500 to 1600 m Maximum speed 80 m/s Guidance system wire Steering system control surfaces Launch platform Individual, Vehicle

minor revision adapted for Luna E-6 series space probes where the guidance system for the entire launch vehicle was moved to the probe itself. Length:

>60 nmi (110 km; 69 mi) Maximum speed 855 km/h (530 mph, 0.698 Mach) Guidance system Inertial navigation system Global Positioning System Infrared homing

millimetric wave new fuse), six fixed wings and the radio receivers. The guidance system is Command Line of Sight (CLOS). It uses a TX antenna installed on

Two-stage: solid-fuel booster and liquid fuel sustainer Operational range 150 km Guidance system Inertial with command updates Accuracy 50 m – 150 m CEP

(366 m) to 1,000 yards (914 m) Warhead Minol Warhead weight 94 kilograms (207 lb) Detonation mechanism Proximity and/or time Guidance system Type 170 sonar

fragmentation Engine Solid-fueled rocket motor Operational range >28 km Guidance system Semi-active laser guidance, imaging infrared and millimeter-wave active

that employed the semi-automatic command to line of sight (SACLOS) guidance system instead of the less reliable manual command to line of sight (MCLOS)

in the U.S. Military were surprised the Snark, due to its dubious guidance system, was ever operational. The most accurate of the seven full-range flights

Pilots would set their onboard navigation systems to fly the Instrument Guidance System (IGS) path straight towards a large red and white checkerboard on the

Kerosene Operational range 50 km Flight altitude 50 m (cruising) 5 m (terminal) Maximum speed Mach 2 Guidance system Radar Launch platform Air, surface

87–90 kg HE blast/fragmentation Operational range 15-120 km Maximum speed Mach 3.5 Guidance system Passive/anti-radiation Launch platform Air launched

km (MK3) Flight altitude sea skimming Maximum speed high subsonic Guidance system pulse-laser, passive IR (MK2), passive IR, radar altimeter (MK3) Launch

on electrical signals from the gyros. The Siemens Vertikant LEV-3 guidance system consisted of two free gyroscopes (a horizontal for pitch and a vertical

used on earlier missiles. The R-5, for instance, used an inertial guidance system that had to be "fine tuned" by commands from ground radio stations

stronger airframe than the standard Thor IRBM and had the inertial guidance system replaced by a radio guidance package mounted on the Able stages. It

rocket Operational range DF-11：300+ km DF-11A：700+ km DF-11AZT：600 km Guidance system Astro-inertial guidance (including ring-laser gyroscope) + Beidou satellite

test vehicles began. These included live ramjets, but still had no guidance system or warhead. The designation YF-99A had been reserved for the operational

9 in) Armor 10mm maximum Main armament 330 kg (730 lb) explosive Engine 1.5L Opel Olympia Suspension torsion bar Guidance system wireless, up to 2 km

very small targets such as cruise missiles or UAVs triple-channel guidance system for more robust countermeasure rejection improved engine to provide

of conventional explosive. The guidance systems consist of inertial guidance system and global positioning system. Hyunmoo-3A, which was nicknamed "Eagle-1"

decision to change from the preset guidance of the V-1 to a command guidance system utilizing a radar beacon in the missile and radio command guidance

produced components, such as LE-5 engine on the second stage and inertial guidance system, the most crucial part, the first stage engine, was a licence-built

comes in two versions. The first one which only has radio command guidance system and the other one which has GPS guidance and IR emissions. Both versions

Engine Turbofan Operational range 240 km (130 nmi) 400 km (220 nmi) (Upgraded version) Maximum speed subsonic Guidance system GPS and inertial guidance

blast-fragmentation Engine Solid fuel rocket Operational range 75 km (47 mi) Maximum speed Mach 4 Guidance system Semi-active radar homing Launch platform aerial

gimbals was controlled by gyroscopic inertial reference; this type of guidance system was invented by Robert H. Goddard amongst others, who had partial success

psychologists Jack Loomis and Roberta Klatzky) of the UCSB Personal Guidance System. B.A. (Honors), University of New England (Australia), 1959 M.A., University

differed from the DC-130As in having a chin radome containing a microwave guidance system in addition to the nose thimble radome which housed tracking radar

guidance package made by AC Spark Plug was replaced by a radio ground guidance system, which was mounted to the second stage instead of the first. NASA made

Engine Liquid-propellant rocket Operational range 45–75 mi (72–121 km), depending on warhead Maximum speed >Mach 3 Guidance system inertial guidance

and destroy at least sixty percent of the attacking force. The dual guidance system ensures protection against electronic countermeasures and operation

10 m (33 ft) (terminal) Maximum speed Mach 3 (0.6 mi/s; 1.0 km/s) Guidance system Inertial measurement unit (IMU) and active radar seeker Launch platform

(RIM-24C) Flight ceiling 50,000 ft (15 km) (RIM-24A) 65,000 ft (20 km) (RIM-24B) Maximum speed Mach 1.8 Guidance system SARH Launch platform Surface ship

worked as a carpenter. The company's first product was called the "AI Guidance System", which began development in 2016 and was first brought to market in

5 mi) Flight altitude 5.5 km (18,000 ft) Maximum speed Mach 2.1 (720 m/s (1,600 mph)) Guidance system Radar CLOS guidance Launch platform Surface Ship

Operational range 2 to 25 kilometres (1.2 to 15.5 mi) Maximum speed Mach 1.6 Guidance system Semi-active radar homing (R-4R) Infrared homing (R-4T) Launch platform

following the 7 July 2005 London bombings Europe's largest Dynamic Route Guidance System, in Nuremberg, Germany (hybrid rotating prism and row matrix LED) A

instruction fetch and instruction issue Saturn V instrument unit, a guidance system for the Saturn V rocket International unit, a unit for biological activity

more cost-effective and allows the use of simpler electronics in the guidance system.  Australia  Iran  Iraq  Romania  Philippines  Singapore  Slovakia

determined that an unknown source of low frequency noise had caused the guidance system to order course corrections when none were needed, causing the steering

rocket Operational range 100 mi (87 nmi; 160 km) Maximum speed Mach 4 Guidance system Semi-active radar homing, terminal infrared homing Launch platform

Solid fuel rocket Operational range 18 km Maximum speed 2695 km/h Guidance system Semi-active radar homing (PL-4A) Infrared homing (PL-4B) Launch platform

the Netherlands, while Belgium was to develop the downrange ground guidance system. By 1969, the ELDO was beginning to realize that dividing work up by

Aviation Industries Organization Specifications Warhead HE Engine turbojet Operational range 25 km Flight altitude Sea-skimming Guidance system Active radar

100 km) Maximum speed Approximately 15,000 miles per hour (Mach 20; 24,000 km/h; 6.7 km/s) (terminal phase) Guidance system Inertial Launch platform Silo

test range support. The Scalpel Plus version has a dual-mode SAL/GPS guidance system. Weight: 100 lbs (45.3 kg) Length: 75 in (1905 mm) Diameter: 4 in (102 mm)

Force Production history No. built 0 Specifications Warhead 10–20 MIRV Engine Solid fuel rocket Guidance system Inertial Launch platform Silos, railway

Yemeni origin. Elements of the missile's design, including the inertial guidance system, fins, and control surfaces, are identical to those of the Qiam 1,

programmed into the D37D computer, which contained a hybrid explicit guidance system for the first time. A new class of program was required by the Joint

Propellant liquid fuel Operational range 200 km Maximum speed Mach 0.85 Guidance system CCD/TV-seeker for KD-88 or imaging infrared (IIR) for KD-88A Launch

tracking range of 40 km. System weight is 8 tons. The Lev-218 (MR-184) guidance system was developed by KB Ametist on the basis of Lev-114: (MR-114 from the

(missile) Range: 500 m to 6000 m Altitude: 10 m to 4000 m Overload: ≥18 g Guidance System: Infrared homing/Ultraviolet dual-spectrum seeker HN-6 is a further

Operational range 1,770 km (JL-1), 2,500 km (JL-1A) Flight altitude 500 km Guidance system Inertial Accuracy 700 meters (JL-1) and 100 meters (JL-1A) Launch platform

launch pad. It had been a long and difficult road to develop the L1 guidance system, but it worked perfectly that time. Zond 6 flew around the Moon on

Sukhoi Su-30MKM. KAB-500S-E is a Precision-Guided Munition (PGM) whose guidance system is based on GLONASS. The weapon can be dropped from aircraft flying

feet (17 km). The first Model 147A was a standard Firebee with a new guidance system consisting of no more than a timer-programmer, a gyrocompass, and an

missiles' transporter launchers, and some 90% of the components of the guidance system were manufactured in Ukraine. In Belarus, as of December 1995, 63 RT-2PM

modified version of the missile, with improved GPS-based navigation and guidance system and longer range, however the MA-31 program went no further, and the

Unit cost Unknown Specifications Warhead 3 Conventional warheads Engine Liquid Operational range Unknown (estimated 2,500 km) Guidance system Inertial

Effective firing range 4000 yards Warhead HBX Warhead weight 500 pounds Engine Electric Maximum speed 29 knots Guidance system Gyroscope Launch platform Submarines

7000 yards Warhead Mark 36, HBX-1 Warhead weight 800 pounds Engine Electric Maximum speed 47 knots Guidance system Gyroscope Launch platform Submarines

patience in addition to pure trial and error. A complete shuttle guidance system is included in the game's instruction manual. Finally, the player must

of the Dietary Guidelines and MyPyramid for Americans and the Food Guidance System. Hentges joined USDA with over 20 years of experience in nutrition

software, announced in 2015 that they had been able to optimise the guidance system by fine-tuning its predicted line of sight. An effective range of 800 m

Alpha Mission: Missile Hangar The objective is to retrieve a missile guidance system that is held inside a hangar currently used by a terrorist group. They

solid-propellant rocket Operational range 20 km (12.4 mi; 10.8 nmi) Guidance system Multi-element imaging infrared (IIR) Active radar seeker Launch platform

190 km) (actual range is classified) Speed: 3,000+ mph (4,680+ km/h) Guidance system: semi-active and active radar homing Warheads: proximity fuze, high

silver-zinc oxide batteries Maximum speed 35 knots (65 km/h; 40 mph) Guidance system wire-guided and passive terminal homing Launch platform SHIP , submarines

cm Warhead Up to three Engine Solid-fuel rocket Operational range 34–45 km Maximum speed 750 m/s Guidance system None Accuracy In excess of 500 m CEP

2014 Produced Unknown Variants Fajr-4 Fajr-4CL Specifications Diameter 333 mm Guidance system Onboard guidance Launch platform Sukhoi Su-22 References

range 250–270 nmi (290–310 mi; 460–500 km) Maximum speed Mach 2.5 to 4 Guidance system BeiDou satellite navigation with mid-course updates, terminal active

(840 TJ) Engine Thiokol XM100 200 kN (45,000 lbf) Propellant Solid fuel Operational range 75 nmi (139 km) Boost time 34 sec Guidance system Inertial

capability to evade missile defence systems. It is based on terminal guidance system technology, which improves warhead accuracy by firing small thrusters

range of about 1.5 km (0.93 mi). It used a Kehl-Straßburg MCLOS radio guidance system (the Funkgerät FuG 203-series Kehl transmitter in the launching aircraft

(120 mi) Warhead High explosive blast-fragmentation Maximum speed Mach 5 Guidance system Inertial guidance, two way data link, active radar homing Launch platform

23:34 Atlas C 4C CCAFS LC-12 ICBM test Suborbital Partial failure Guidance system failure T+80 seconds, however the flight control system kept the missile

contact exploder Engine Contra-rotating turbine Maximum speed 26 knots Guidance system gyroscope Launch platform battleships, torpedo boats and cruisers

1967 21 18 3 The only operational ICBM version. Improved range and guidance system. Only 6 launch positions were available. Used as a base for 11A57 and

was an early precursor to the Zvezda and M-40 Buran projects. The guidance system was realized using an inertial system and also a star tracking system

the missiles. But the Hae Ryong was fitted with a semi-active laser guidance system, limiting its tactical capability during bad weather. Additional pressure

are also often found on "smart" or guided munitions as an aid to the guidance system. By stabilizing the slipstream of air traveling over the weapon, the

<42 km 128 km (CM-708UNA) 290 km (CM-708UNB) Maximum speed Mach 0.9 Guidance system Inertial navigation/active radar homing terminal guidance Launch platform

environment, thus supplementing the position sensing GPS system. An internal guidance system utilizing gyroscopes and accelerometers monitored the orientation of

Belarus for its guided version, it was estimated that the Inertial guidance system for the guided version would allow the missile to achieve a CEP of

Shahin-2:20 km Maximum speed Shahin-1:450 m/s max Shahin-2:660 m/s max Guidance system Unguided, ballistic flight Launch platform unarmored rail launcher

missile, AR-2 missile (20 kg, 5 kg armour-piercing warhead, inertial guidance system with terminal semi-active laser (SAL) seeker, maximum range 8 km),

ft) Warhead weight 435 kg (960 lb) Operational range 210 km (130 mi) Guidance system Radar seeker (later anti radiation missile version) Launch platform

6,370–6,500 kg Length 11.37–12.29 m Diameter 0.885 m Warhead 770kg Engine Liquid Operational range 500 km Guidance system inertial Accuracy 500m CEP

20/90/150kt Propellant Solid-fuel rocket Operational range 7,200 km (4,500 mi) Guidance system Astro-inertial with Beidou Launch platform Type 094 submarine

eliminating the Snark, but in its report recommended only that the Snark's guidance system be simplified and that development continue. Members contended that

of the Minuteman II, an ICBM with increased range and an improved guidance system. In the 1980s, Whiteman AFB became the first missile base to field

in an electrical circuit Precision approach radar, a radar aircraft guidance system All pages with titles beginning with Par All pages with titles containing

ceiling 4.5 km (15,000 ft) Maximum speed Up to 500 m/s (Mach 1.5) Guidance system Three-channel optical seeker (ultraviolet, near-infrared, mid-infrared)

glider Terminal: solid rocket engine Flight altitude 2 m (6 ft 7 in) Guidance system Gyroscopic autopilot; instrumented feeler probe, radar altimeter. Launch

fuse Propellant Solid propellant Operational range 50 km Flight ceiling 25-27 km(75000 ft) Guidance system Active radar homing Launch platform Ra'ad

rocket Operational range 18,044 yd (16.5 km) Maximum speed Mach 2.3 Guidance system Narrow-band passive radar seeker Launch platform AV-8B Harrier AH-1

rocket Operational range 23 kilometres (14 mi) Maximum speed Mach 2 Guidance system Semi-active radar homing (R-98MR) Infrared homing (R-98MT) Launch platform

range 17.3 nmi (32.0 km) Flight ceiling 80,000 ft (24,000 m) Maximum speed Mach 3.0 Guidance system Semi-active radar homing Launch platform Surface ship

SA-N-1B. The Neva-M introduced a redesigned booster and an improved guidance system. The S-125 was not used against U.S. forces in Vietnam, because the

rocket, testing technologies needed for the Tronador II, which has a guidance system and would be capable of reaching low Earth orbit. Development of the

Flight ceiling 15–21.5 km (9–13 mi) Maximum speed Mach 1.6 to 2.5 Guidance system Nitrogen cooled passive InPb infrared seeker Launch platform aerial

the target without further operator intervention (using an inertial guidance system, it can generally keep the laser on target even if the beam is temporarily

mechanism Mk 19 Mods 4 and 11 contact exploder Engine Electric Maximum speed 12 knots Guidance system Helix search Launch platform Destroyers and aircraft

solid-fuel rocket engine Operational range 9 km (5.6 mi) Maximum speed 5,040 km/h (3,130 mph) Guidance system SARH Launch platform Mikoyan-Gurevich Ye-152A

Effective firing range 30–50 km Maximum firing range Up to 50 km Flight altitude 14 km Guidance system Inertial guidance/GLONASS Launch platform Aircraft

navigation. Vega has been in business since 1972 when it built a marine guidance system based on a design by Norman Rumsey. Throughout the forty-plus years

guidance or GPS to follow a preset course; once over land, the missile's guidance system is aided by terrain contour matching (TERCOM). Terminal guidance is

motor Operational range 50–80 km (31–50 mi) Maximum speed Mach 2.2-4.5 Guidance system Inverse monopulse Semi-active radar homing (R-40RD) Infrared homing

Liquid fuel Operational range 1000 km Maximum speed 185 km/h (115 mph) Guidance system EO, inertial, and anti-radiation homing Launch platform Box launcher

IMProvement) which saw the replacement of six old circuit cards in the guidance system with one, allowing the spare volume to be used for an autopilot. Used

Operational range 42 km Flight altitude 5 or 7 m Maximum speed ≈ Mach 0.9 Guidance system Inertial navigation/active radar homing terminal guidance Launch platform

IMProvement) which saw the replacement of six old circuit cards in the guidance system with one, allowing the spare volume to be used for an autopilot. Used

contact detonation Engine Electrical batteries Maximum speed 35 knots (65 km/h) Guidance system Wire-guided with autonomous active terminal homing sonar

3–16km (PL-5B, PL-5C), 0.5-16~18km (PL-5E) Maximum speed Mach 2.5 Guidance system Infrared homing, multi-element, dual band detector(PL-5EII) Launch

FGM-172A: proximity fuze FGM-172B: combined contact fuze & time fuze Guidance system PLOS (Predicted Line Of Sight) Launch platform Man-portable launcher

Manufacturer Northrop Corporation Specifications Diameter 2.75 inches (70 mm) Engine Thiokol TRX-126B Propellant Solid fuel Guidance system Unguided

engines) with an Agena D upper stage, though without the all-inertial guidance system, malfunction detection equipment, and redundant systems required for

scramjet), kerosene Operational range 3000-4000 km Maximum speed Mach 5+ Guidance system inertial, TERCOM , GLONASS , Radar , IR IIR , TV camera , Opto-Electronic

technician who had accidentally transposed two wiring connectors in the guidance system, causing pitch errors to be interpreted as yaw errors and vice versa

Instruments Telescope assembly (TA) Ariel infrared spectrometer (AIRS) Fine Guidance System (FGS) Ariel mission insignia Cosmic Vision ← PLATO EnVision →

possibility that the bombing was the result of a failure in the bombs guidance system rather than being the result of pilot error. Kajaki has a hot desert

Commission (SUPARCO) during the time of the development of Shaheen missile guidance system. SUPARCO is a Pakistani governmental agency. His death led to the mass

000 kilometres (1,900 mi) Reduced load: ~4,000 kilometres (2,500 mi) Guidance system: Inertial navigation system with GPS/NavIC satellite guidance Circular

Length 8 m Diameter 610 mm Warhead one Engine Solid Operational range 210 km (130 mi) Guidance system None Launch platform Transporter erector launcher

which allow for flexible targeting. The missile also has an internal guidance system that allows it to find its way to the target on its own after launch

Autonomous underwater vehicle – Uncrewed underwater vehicle with autonomous guidance system Argo floats – International oceanographic observation program Liquid

pounds Detonation mechanism Mk 14 Mod 2 contact exploder Engine Electric Maximum speed 19.6 knots Guidance system Gyroscope Launch platform Submarines

maintenance fees. HRH has added the Mazor Robotics Renaissance Surgical Guidance System to its spine surgery program and is the exclusive provider of Mazor

7 in) Engine Three-stage solid propellant Operational range 10,000 km Guidance system autonomous inertial guidance Accuracy Maximum error: 4 km, CEP: 1900

the gas to escape and was attached to a long stick that acted as a guidance system for flight direction control. The first rockets with tubes of cast

(31 mi) Maximum speed Mach 7.5 (9,190 km/h; 5,710 mph; 2.55 km/s) Guidance system Ring laser gyro inertial navigation system and accelerometer Accuracy

RD-68 Second Stage: 1x RD-219 + 1x RD-69 Propellant AK27I + UDMH Operational range 11,000–13,000 km Guidance system inertial guidance Accuracy 2.7 km

Subcontractors included the Sperry Gyroscope Company who produced the missile guidance system whilst the nuclear warhead was designed by the Atomic Weapons Research

kilometres (1.2 to 3.7 mi) Maximum speed 2,880 km/h (1,790 mph) (Mach 2.33) Guidance system beam riding Launch platform MiG-17, MiG-19, MiG-21, Su-9

In May 1996, trials of the Aster 15 active electromagnetic final guidance system against live targets began. All six attempts were successful. During

Specifications Warhead HEAT and others Operational range 10 km (6.2 mi) Guidance system fiber-optic wire-guided missile (AFT-10) Infrared homing Launch platform

engine Operational range from 1000 km to 10250 km with MIRV 10320 km with single warhead Guidance system inertial Accuracy CEP 500 metres at 10000 km

10.94 m Diameter 0.885 m Warhead 1,000 kg Operational range 350 km Guidance system Inertial Accuracy approximately 450m circular error probable (CEP)

stage, solid fuel rocket Operational range 300 km Maximum speed Mach 4 Guidance system Inertial & electro-optical terminal (according to Iranian state media)

rocket Operational range 35–45 km (22–28 mi) Maximum speed Mach 0.9 Guidance system Inertial guidance Launch platform Akula, Oscar, Typhoon, Alfa, Delta

Length 4m Diameter 0.35m Engine Turbojet engine Operational range 180km Flight altitude 5-6m Guidance system Inertial and active radar Launch platform Air

6000 yards Warhead Mk 26 Warhead weight 900–1000 pounds Engine Electric Maximum speed 40 knots Guidance system Gyroscope Launch platform Submarines

distinctive square fuselage.[citation needed] It differed primarily in its guidance system (semi-automatic command to line of sight) and the use of an infrared

Warhead HBX Warhead weight 500 pounds Engine Electric Maximum speed 12.5-18.5 knots Guidance system Gyroscope Launch platform Submarines and aircraft

and sustainer Operational range 400 m - 2 km Maximum speed 100 m/s Guidance system MCLOS wire Steering system trailing edge wing spoilers Launch platform

to 2.5 kilometres (0.31 to 1.55 mi) Maximum speed 160 m/s (360 mph) Guidance system Radio command Steering system MCLOS Launch platform Mi-4, Mi-8, Mi-24

fuel rocket Operational range 27 nmi+ (50 km+) Maximum speed Mach 4+ Guidance system Mid-course update datalink Terminal semi-active radar homing for Block

In 1993, the UCSB group first publicly demonstrated the Personal Guidance System (PGS) using a bulky prototype carried in a backpack. Since then, they

excessive altitude and insufficient velocity. This prevented the normal guidance system cutoff commands from being sent so SECO was caused by propellant depletion

thrust for 4 sec. Maximum speed 900–1,000 km/h (560–620 mph; 490–540 kn) Guidance system MCLOS; visual guidance by telescope, radio controls; two-man crew

telescope axis. Two additional sidereal spectrographs. Three-axes guidance system accuracy: better than 5 arcsec on two cross-sectional axes of telescope

actuator and gyroscope were the main components of the control and guidance system of the missile. The actuators were spoiler type, (similar to Mosquito

place. The M1128 is expected to be compatible with a nose-mounted guidance system—specifically, the XM1156 Precision Guidance Kit, which fits the standard

triggered Engine Solid Rocket Motor, 2-stage Flight ceiling 6 km Maximum speed 930 m/s, approx. Mach 2.71 (high supersonic) Guidance system Infrared homing

worked as an electrical engineer on the abort guidance system of the Apollo Program. The abort guidance system was used during the Apollo 13 mission to safely

J402-CA-100 turbojet 674 lbf (3 kN) Operational range 230 mi (370.4 km) Guidance system GPS, INS, IIR Steering system Moving wings & 2 tailplanes Accuracy

to Starstreak) which would maintain the use of a laser beam-riding guidance system as means of overcoming the tight rules of engagement present in in-shore

Effective firing range 1,650 to 26,750 yards (1,510 to 24,460 m), depending on launch altitude Guidance system Electro-optical Accuracy 20 ft (6.1 m) CEP

10.3 m Width 0.68 m Propellant Single-stage Solid-propelled Operational range 700 km Guidance system INS, GPS Accuracy 100 m CEP estimated References