The procedure of choosing the best solution for a space carrier rocket for the 90's is depicted. The aim is the deposition of nuclear wastes in space. All rockets have a nominal weight of 1000 t. One and two stage rockets were studied. The equipment may be lost during each flight or partially or fully reused. All technical and cost requirements were investigated and the results are tabulated for the different choices.
Future Satellite Carriers Zukuenftige Satellitentraeger
1981
41 pages
Report
Keine Angabe
Englisch
Zukuenftige Fahrzeugsicherheit
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