Propulsion technology challenge - an abortable, continuous use vehicle

Propulsion technology challenge - an abortable, continuous use vehicle

The various aspects of the design and construction of an abortable, continuous use space vehicle are discussed and the different propulsion characteristics required, as well as the technology necessary to provide those characteristics are described. It has been suggested that the next century's...

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Veröffentlicht in:Acta astronautica 1996, Vol.38 (4-8), p.235-249
Hauptverfasser: Czysz, Paul A, Froning, H David
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Sprache:eng
Schlagworte:
Rocket engines
Social aspects
Space flight
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container_title Acta astronautica
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creator Czysz, Paul A
Froning, H David
description The various aspects of the design and construction of an abortable, continuous use space vehicle are discussed and the different propulsion characteristics required, as well as the technology necessary to provide those characteristics are described. It has been suggested that the next century's orbital operations should not be based on an expendable rebuilt for reuse concept but on a rocket based combined cycle engine based on those now in space operation.
doi_str_mv 10.1016/0094-5765(96)00043-4
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subjects Rocket engines
Social aspects
Space flight
title Propulsion technology challenge - an abortable, continuous use vehicle
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