The paper presents launch vehicle and upper-stage options for application to lunar and interplanetary microspacecraft missions. Particular attention is given to the capabilities of Piggyback, small launch vehicles, and large launch vehicles. It is noted that Piggyback options on the Shuttle and expendable launch vehicles enable near-term earth-orbital missions and the potential for lunar and planetary missions if an electric-propulsion upper-stage is developed. Launch systems like the Space Shuttle could be used to launch large members of microspacecraft in 'constellation deployment' and 'shotgun' class missions to a variety of solar-system targets such as the sun, asteroids, comets, the moon, Mars, and Saturn.
Chemical launch system options for microspacecraft
1989-10-01
Sonstige
Keine Angabe
Englisch
Microspacecraft Attitude Control
NTRS | 1992
|Innovative, low cost microspacecraft
AIAA | 2000
|NTRS | 1992
|