gravity gradient attitude

gravity gradient attitude
gravity orientation, gravity gradient attitude
ГО, гравитационная ориентация

English-Russian dictionary of program "Mir-Shuttle". . 2015.

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  • Attitude dynamics and control — The attitude of a body is its orientation as perceived in a certain frame of reference; providing a vector along which a spacecraft is pointing is a description of its attitude. Dynamics is the term for the modeling of changing conditions, due to …   Wikipedia

  • Transit Research and Attitude Control — The Transit Research and Attitude Control (TRAAC) satellite was launched by the U.S. Navy from Cape Kennedy along with Transit 4B on November 15, 1961. The 109 kg satellite was used to test the feasibility of using gravity gradient stabilization… …   Wikipedia

  • Mir — This article is about the Soviet/Russian space station. For other uses, see Mir (disambiguation). Mir …   Wikipedia

  • STS-51-B — Infobox Space mission mission name = STS 51 B insignia = Sts 51 b patch.png shuttle = Challenger launch pad = 39 A launch = April 29, 1985, 16:02:18 UTC landing = May 6, 1985, 16:11:04 UTC Edwards AFB, Runway 17 duration = 7d/00:08:46 altitude =… …   Wikipedia

  • Control moment gyroscope — A control momentum gyroscope (CMG) is an attitude control device generally used in spacecraft attitude control systems. A CMG consists of a spinning rotor and one or more motorized gimbals that tilt the rotor’s angular momentum. As the rotor… …   Wikipedia

  • Badr-B — Infobox Spacecraft Name = Badr B Organisation = SUPARCO Mission Type = Earth Observation Satellite Satellite Of = Earth Launch = December 10 2001, 17:19 UT Carrier Rocket = Zenit 2 NSSDC ID = 2001 056C Webpage = Mass = 68.0 kg Power = Orbital… …   Wikipedia

  • Momentum exchange tether — Momentum Exchange Tethers is one of many applications for space tethers. This sub set represents an entire area of research using a spinning conductive and/or non conductive tether to throw spacecraft up or down in orbit (like a sling), thereby… …   Wikipedia

  • Tether propulsion — systems are proposals to use long, very strong cables (known as tethers) to change the velocity of spacecraft. The tethers may be used to initiate launch, complete launch, or alter the orbit of a spacecraft. Spaceflight using this form of… …   Wikipedia

  • STS-99 — Infobox Space mission mission name = STS 99 insignia = Sts 99 patch.png shuttle = Endeavour launch pad = 39 A launch = February 11, 2000, 12:43 p.m. EST (17:43 UTC) landing = February 22, 2000, 6:23 p.m. EST, KSC, Runway 33 duration = 11 days, 5… …   Wikipedia

  • Soyuz 29 — Infobox Space mission mission name = Soyuz 29 sign = Photon crew members = 2 launch pad = Gagarin s Start launch = June 15, 1978 20:16:45 UTC landing = September 3, 1978 11:40:34 UTC 46° N, 69° E duration = 79d/15:23:49 apogee = 266 km perigee =… …   Wikipedia

  • Soyuz T-5 — Infobox Space mission mission name = Soyuz T 5 sign = Эльбрус (Elbrus) crew members = 2 (at launch) 3 (at landing) launch = May 13, 1982 09:58:05 UTC Gagarin s Start landing = August 27, 1982 15:04:16 UTC 225 km E of Dzhezkazgan duration =… …   Wikipedia


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