Orbit transfer vehicles (OTV) are evaluated against mission model requirement. Mission suitability of OTVs using storable propellant, cryogenic propellant, and electric propulsion systems is outlined. Energy required, g-level, spacecraft deploy/return, operational constraints, mission duration, and packaging are considered.
Storable orbit transfer vehicle
01.06.1982
Aufsatz (Konferenz)
Keine Angabe
Englisch