With increasing transport requirements, reusable space transporters again receive serious consideration in Europe as successors to the Ariane family. The paper deals with a hydrogen-ramjet-propelled, 1-1/2-stage reusable ballistic space transporter with vertical take-off and landing and using liquid hydrogen/oxygen rockets. This novel concept was developed in a theoretical study at the University of Stuttgart. The results are compared with recently published studies of several other European space transporter concepts. The data derived for the Istra - concept are: 15.4 Mg payload into low Earth-orbit, 155 Mg gross lift-off mass, 10% payload ratio, which represents a 57% propellant saving, and 44% reduction in dry mass (structure and engines) compared with comparable two-stage pure rocket concepts.
An air-breathing ballistic space transporter for Europe
Ann. Conv. of the DGLR ; 1982 ; Stuttgart, Germany
01.03.1985
Aufsatz (Konferenz)
Keine Angabe
Englisch
Air-Breathing Ballistic Space Transporter for Europe
NTIS | 1985
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