The feasibility of constructing a small inexpensive subsatellite for use in connection with the space shuttle program is discussed. The satellite is designed to carry out various scientific experiments in orbits that are independent of the main space laboratory. A modular concept characterizes the design. Special emphasis was placed on the investigation of orbital mechanics.
Feasibility Study of a Spacelab Subsatellite
1980
246 pages
Report
No indication
English
Manned Spacecraft , Unmanned Spacecraft , Astronautics , Feasibility analysis , Satellite design , Satellite-borne instruments , Space shuttles , Mission planning , Propellant tanks , Recoverable spacecraft , Satellite configurations , Satellite orbits , Spacecraft modules , Spacecraft power supplies , Spacelab , Foreign technology , Translation