Multiple payload Shuttle flights from WTR - Some operational and orbital mechanics considerationsIt is pointed out that if the difference between the nodal crossing time of the Shuttle parking orbit and the final orbit of a spacecraft is more than about half an hour, current design spacecraft may have to carry a prohibitively large propulsion system to meet its requirements. Various solutions to this problem are discussed.
Document ID
19810062896
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Edgecombe, D. S. (Battelle Columbus Labs. OH, United States)
Fischer, N. H. (Battelle Columbus Labs. OH, United States)
Rea, F. G. (Battelle Columbus Laboratories Columbus, OH, United States)