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Apogee motor is a redirect to apogee kick motor

searching for Apogee motor 29 found (169 total)

Koreasat 1 (275 words) [view diff] exact match in snippet view article find links to article

satellite was equipped with a Star 30 solid apogee motor. It carried 625 kg (1,378 lb) of fuel for the apogee motor and 187 kg (412 lb) of hydrazine propellant

Sirius FM-5 (280 words) [view diff] exact match in snippet view article find links to article

will raise itself into geostationary orbit by means of its onboard R-4D apogee motor. It also carries four SPT-100 engines for manoeuvring. It is the first

GSAT-2 (397 words) [view diff] case mismatch in snippet view article find links to article

Weighing 1800 kg at launch, GSAT-2 incorporated a 440 newton Liquid Apogee Motor (LAM) and sixteen 22 newton Reaction Control Thrusters for raising the

INSAT-4E (838 words) [view diff] case mismatch in snippet view article find links to article

motors on board the GSAT-6 satellite. The GSAT-6 satellite's Liquid Apogee Motor (LAM) was fired for 3385 seconds at 08:35 hours IST on August 28 during

GOES 5 (381 words) [view diff] exact match in snippet view article find links to article

itself to geostationary orbit on 2 June by means of an onboard Star 27 apogee motor. Following insertion into geostationary orbit, GOES-5 was briefly placed

Galaxy 11 (572 words) [view diff] exact match in snippet view article find links to article

it raised itself to a geostationary orbit by means of an onboard R-4D apogee motor. Its insertion into geosynchronous orbit occurred at 16:30 on 2 January

GOES 2 (423 words) [view diff] exact match in snippet view article find links to article

it raised itself to geostationary orbit by means of an onboard SVM-5 apogee motor. Its insertion into geosynchronous orbit occurred at 03:26 GMT on 17

IRNSS-1H (907 words) [view diff] case mismatch in snippet view article find links to article

Nitrogen (MON-3) as oxidizer. Twelve 22N thrusters. One 440N Liquid Apogee Motor (LAM) Two 390 litres propellant tanks One 67 litre pressurant tank with

Intelsat 805 (120 words) [view diff] exact match in snippet view article find links to article

a geosynchronous transfer orbit. Intelsat 805 subsequently fired its apogee motor to achieve geostationary orbit. Spaceflight portal McDowell, Jonathan

IRNSS-1C (352 words) [view diff] case mismatch in snippet view article find links to article

raising operation of IRNSS-1C is successfully completed by firing the Apogee Motor for 1,563 seconds. The current orbital parameters are: Animation of IRNSS

Skynet 5B (430 words) [view diff] exact match in snippet view article find links to article

transfer orbit with 6 degrees of inclination. The satellite used its apogee motor to raise itself into geostationary orbit. It is located at a longitude

AMOS-1 (satellite) (533 words) [view diff] exact match in snippet view article

Weighing 970 kg at launch, AMOS-1 incorporated a 400 newtons liquid apogee motor and fourteen reaction control thrusters, each delivering ten newtons

GOES 6 (376 words) [view diff] exact match in snippet view article find links to article

raised itself to geostationary orbit by means of an onboard Star 27 apogee motor, with insertion occurring on 9 May 1983. Following insertion into geosynchronous

GOES 4 (449 words) [view diff] exact match in snippet view article find links to article

raised itself to geostationary orbit by means of an onboard Star-27 apogee motor. Its insertion into geostationary orbit occurred at 12:00 on 11 September

NSS-806 (523 words) [view diff] exact match in snippet view article find links to article

entering a geosynchronous transfer orbit. NSS-806 subsequently fired its apogee motor to achieve geostationary orbit. In July 2017, seven years past its 12-year

GSAT-6A (973 words) [view diff] case mismatch in snippet view article find links to article

GSAT-6A was carried out as planned on 30 March 2018 by firing the Liquid Apogee Motor (LAM) for 2188 seconds from 09:22 AM IST. The second orbit raising maneuver

CMS-02 (403 words) [view diff] case mismatch in snippet view article find links to article

panels 2 × 180Ah Li-Ion battery 16 × bipropellant thrusters 440N Liquid Apogee Motor (LAM) with area ratio of 250 2 × 1207 litre propellant tank 2 × 67 litre

ConeXpress (251 words) [view diff] exact match in snippet view article find links to article

consisted of a capture tool that inserts a probe into the throat of the apogee motor of the Client satellite, locks itself to the throat by expanding the

List of Intelsat satellites (1,014 words) [view diff] exact match in snippet view article find links to article

26 October 1966 23:05:00 Delta E1 Cape Canaveral, LC-17B — Retired — Apogee motor failed, but satellite operated from geostationary transfer orbit (GTO)

GOES 3 (590 words) [view diff] exact match in snippet view article find links to article

which it raised itself to geostationary orbit using an onboard SVM-5 apogee motor. Its insertion into geosynchronous orbit occurred at 03:22 on 17 June

Mars Orbiter Mission (8,962 words) [view diff] exact match in snippet view article find links to article

days after the arrival of NASA's MAVEN orbiter. The 440-newton liquid apogee motor was test fired on 22 September at 09:00 UTC for 3.968 seconds, about

INSAT-3DS (275 words) [view diff] case mismatch in snippet view article find links to article

environment friendly white fairing. Five days later, all four planned Liquid Apogee Motor (LAM) firings were completed. The spacecraft is now in the geosynchronous

Lunar Lander (spacecraft) (2,097 words) [view diff] case mismatch in snippet view article

touchdown". ESA. Retrieved 10 April 2012. "500 N Bipropellant European Apogee Motor (EAM)". Astrium. Archived from the original on 5 April 2012. Retrieved

IHI Corporation (1,301 words) [view diff] exact match in snippet view article find links to article

solid rocket booster for H-IIA/H-IIB Launch Vehicle BT-4 liquid-fuelled apogee motor (used in the Cygnus vehicle which are launched on Atlas V and Antares

Gaganyaan (8,791 words) [view diff] exact match in snippet view article find links to article

oxidizer and fuel, having five main engines derived from ISRO's liquid apogee motor with 440 N (99 lbf) thrust and sixteen 100 N reaction control system

Symphonie (2,079 words) [view diff] exact match in snippet view article find links to article

hot-gas (bi-propellant) thruster system (Ottobrunn and Lampoldshausen). Apogee motor (bi-propellant) subsystem (Ottobrunn and Lampoldshausen). Mechanical

Chandrayaan-2 (11,920 words) [view diff] exact match in snippet view article find links to article

(180 lbf) liquid main engines derived from ISRO's 440 N (99 lbf) liquid apogee motor. Initially, the lander design employed four main throttle-able liquid

1994 in spaceflight (260 words) [view diff] exact match in snippet view article find links to article

Geosynchronous transfer Technology development In orbit Partial launch failure Apogee motor failed to ignite, some experiments successful 29 August 17:38 Atlas E

1963 in spaceflight (January–June) (167 words) [view diff] exact match in snippet view article

Communications In orbit Spacecraft failure Contact with spacecraft lost following apogee motor firing 19 February 16:33 Scout X-3M Point Arguello LC-D US Air Force