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Three stage rocket vehicle with parallel stagingA three stage rocket vehicle has a large forward propellant tank and a small aft propellant tank axially aligned. Secured to the rear end of the aft propellant tank is an engine mount structure carrying rocket engines. Offset and secured to the propellant tanks is a payload structure. The propellants from the large forward tank are fed into the aft propellant tank. This arrangement enables the vehicle to parallel stage its use of engines and components and results in significant payload capability. The design and components fully utilize existing space shuttle elements and tooling.
Document ID
19840019718
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Marshall, W. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
May 29, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-431886
Patent Number: US-PATENT-4,451,017
Patent Number: NASA-CASE-MFS-25878-1
Accession Number
84N27787
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,451,017|NASA-CASE-MFS-25878-1
Patent Application
US-PATENT-APPL-SN-431886
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