Spacecraft systems |
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Contents
Past and Future Kork and rV R Schindler | 3 |
BIGOT G CNES BretignysurOrge SeineetOise France 79 | 39 |
THOME P G NASA Washington D C U S A | 55 |
Copyright | |
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ablation ablative heat shield ablative materials aerobraking aircraft altitude amplifier antenna Apollo application atmosphere boosters capability capsule chemical components configuration cost cylinder density detection detector Diamant diameter Earth orbit Earth resource electronic environment environmental equipment ESRO ESTrack experiments exploration filter Fraunhofer Fraunhofer line function Gemini Grand Tour heat shield IMIEO initial instrument interplanetary inventories lanceur launch vehicle luminescence lunar lunar surface Mars mass measurements meteoroid mission moteur NASA nuclear operations particle payload performance periapsis phase phenolic photocathode photomultiplier piston planet planetary post-Saturn propellant propergol pyrotechnic pyrotechnic devices radiation radiometer range re-entry reliability Rhodamine rocket satellite Saturn sensors sequential space shown in Fig signal Sisyphus solar solar cells Space acceleration Space Flight space photography space vehicle spacecraft structure subsystem Surveyor techniques temperature thermal thrust tion trajectory utilizing velocity voltage weight