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Apogee motor is a redirect to apogee kick motor

searching for Apogee motor 28 found (166 total)

alternate case: apogee motor

Koreasat 1 (282 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
INSAT-4E (629 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
Galaxy 11 (466 words) [view diff] exact match in snippet view article find links to article
it raised itself to geostationary orbit by means of an onboard R-4D apogee motor. Its insertion into geosynchronous orbit occurred at 16:30 on 2 January
GOES 5 (373 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
GSAT-2 (398 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
GOES 2 (415 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 (896 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 (121 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 (343 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
GOES 6 (368 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
AMOS-1 (satellite) (532 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
GSAT-6A (812 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
GOES 4 (441 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 (524 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
Mars Orbiter Mission (6,659 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
Gaganyaan (3,483 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
ConeXpress (232 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
GOES 3 (597 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
STS-51-A (1,099 words) [view diff] exact match in snippet view article find links to article
Motor Capture Device, ACD), which was inserted into the satellite's apogee motor nozzle by Allen. The satellite's rotation was slowed to 1 RPM, and Gardner
List of Intelsat satellites (828 words) [view diff] exact match in snippet view article find links to article
October 1966 23:05:00 Delta E1 Cape Canaveral, LC-17B N/A Retired N/A Apogee motor failed, but satellite operated from geostationary transfer orbit (GTO)
IHI Corporation (1,072 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
Lunar Lander (spacecraft) (2,071 words) [view diff] case mismatch in snippet view article
touchdown". ESA. Retrieved 10 April 2012. "500 N Bipropellant European Apogee Motor (EAM)". Astrium. Retrieved 5 April 2012. "Astrium investigates automatic
Chandrayaan-2 (10,409 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 (139 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
Symphonie (2,063 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
1963 in spaceflight (January–June) (148 words) [view diff] exact match in snippet view article
Communications In orbit Spacecraft failure Contact with spacecraft lost following apogee motor firing 14 February R-9 Desna Baikonur RVSN RVSN Suborbital Missile test