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Technology needs for single stage to orbit propulsionNASA's Reusable Launch Vehicle (RLV) Propulsion Technologies Program includes maturation and demonstration activities supporting a variety of propulsion system concepts. The primary emphasis of this program is to identify and mature the technologies required to enable the development of the optimum main propulsion system (MPS) for RLV applications. By applying a methodical approach to the maturation process, through use of subscale system and subsystem validation testing and, where appropriate, engine system level technology demonstration, the development cost of the RLV MPS will be substantially reduced. The major building blocks of this approach are Engine Systems and MPS Subsystem Demonstrators, Supporting Component Technologies, and Russian Technologies, are described further.
Document ID
19950002766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stoyanof, S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Monk, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 17, 2013
Publication Date
November 1, 1994
Publication Information
Publication: Pennsylvania State Univ., NASA Propulsion Engineering Research Center, Volume 2
Subject Category
Spacecraft Propulsion And Power
Accession Number
95N70886
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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