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Advanced heavy lift launch vehiclesThe performance requirements of advanced technology-incorporating, next-generation heavy lift launch vehicles (HLLVs) for LEO missions are discussed, and the configurational features facilitated by those technologies are evaluated. These 1990s 'cargo' vehicles will capitalize on advanced avionics, software and automation, novel hot structure and thermal insulation materials, and more powerful liquid-fuel rockets employing either hydrogen or hydrocarbons. The configurations considered include a winged booster. The use of Space Shuttle components is a major cost-minimization strategy in many of these HLLV design efforts.
Document ID
19880047882
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shelton, Billy W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AAS PAPER 86-408
Report Number: AAS PAPER 86-408
Meeting Information
Meeting: Aerospace century XXI: Space flight technologies
Location: Boulder, CO
Country: United States
Start Date: October 26, 1986
End Date: October 29, 1986
Sponsors: AAS
Accession Number
88A35109
Distribution Limits
Public
Copyright
Other

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