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Centaur D1-A systems in a nutshellThis report identifies the unique aspects of the Centaur D1-A systems and subsystems. Centaur performance is described in terms of optimality (propellant usage), flexibility, and airborne computer requirements. Major systems are described narratively with some numerical data given where it may be useful.
Document ID
19870006563
Document Type
Technical Memorandum (TM)
Authors
Gordan, Andrew L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TM-88880
E-3287
NAS 1.15:88880
Funding Number(s)
PROJECT: RTOP 917-60-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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