The microspacecraft is defined as a fully functional spacecraft whose mass is on the order of 10 kg or less. The results of a recent microspacecraft workshop are reviewed. The workshop concluded that microspacecraft are feasible and can be enabling for missions that require multiple simultaneous measurements displaced in position or very high mission delta-VSDIO-s. The paper includes discussions of science objectives and instruments as well as potential missions. Potential missions include a very close approach to the sun, determining the origin of gamma ray bursters and a search for gravity waves. Technology for microspacecraft is coming from the 'Lightsat' or small satellite community and developments sponsored by the SDIO. Concepts for microspacecraft power and telecommunications subsystems developed at the JPL are presented. Due to their small size, microspacecraft can be launched by traditional chemical rockets and also unconventional launchers such as electromagnetic launchers.
Microspacecraft missions and systems
1989-10-01
Sonstige
Keine Angabe
Englisch
Enabling technologies for microspacecraft missions
AIAA | 1999
|Planetary missions using microspacecraft technology
NTRS | 1992
|Power, Propulsion and Communications for Microspacecraft Missions
British Library Conference Proceedings | 1999
|