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Space shuttle with common fuel tank for liquid rocket booster and main engines (supertanker space shuttle)An operation and schedule enhancement is shown that replaces the four-body cluster (Space Shuttle Orbiter (SSO), external tank, and two solid rocket boosters) with a simpler two-body cluster (SSO and liquid rocket booster/external tank). At staging velocity, the booster unit (liquid-fueled booster engines and vehicle support structure) is jettisoned while the remaining SSO and supertank continues on to orbit. The simpler two-bodied cluster reduces the processing and stack time until SSO mate from 57 days (for the solid rocket booster) to 20 days (for the liquid rocket booster). The areas in which liquid booster systems are superior to solid rocket boosters are discussed. Alternative and future generation vehicles are reviewed to reveal greater performance and operations enhancements with more modifications to the current methods of propulsion design philosophy, e.g., combined cycle engines, and concentric propellant tanks.
Document ID
19910018943
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thorpe, Douglas G.
(University of Central Florida Orlando, FL, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: NASA, Washington, Space Transporation Propulsion Technology Symposium. Volume 3: Panel Session Summaries and Presentations
Subject Category
Spacecraft Propulsion And Power
Accession Number
91N28257
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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