NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Weight trends for a fully reusable advanced single-stage shuttleThe rate at which subsystem weights grow with vehicle gross weight is assessed and is shown to be critical to the efficiency of large Earth to orbit transports. The overall trend, however, is a reduction in the inerts as a percentage of gross weight as the vehicle size is increased. For this reason, the larger the vehicle, the greater the payload weight delivered per pound of vehicle manufactured. Other critical issues addressed include the effects of wing loading and wing size on wing weight, the effect of entry planform loading on thermal protection system weight, the impact of power demand on cooling system and prime power weight, and tank fineness ratio on insulation weight. The effects of body shape and various internal packaging arrangements on weight and balance are also discussed. The greatest impact on overall vehicle weight is body shape and internal packaging, and could account for weight savings of up to 30 percent in body structure. Other subsystems are important, but the savings are much smaller in relation to overall vehicle weight--individually less than one percent.
Document ID
19830027789
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Macconochie, I. O.
(NASA Langley Research Center Hampton, VA, United States)
Lemessurier, R. W.
(Kentron International Hampton, Va., United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:85656
NASA-TM-85656
SAWE PAPER-1554
Report Number: NAS 1.15:85656
Report Number: NASA-TM-85656
Report Number: SAWE PAPER-1554
Meeting Information
Meeting: Ann. Conf. of the Soc. of Allied Weight Engr., Inc.
Location: Anaheim, CA
Country: United States
Start Date: May 23, 1983
End Date: May 25, 1983
Accession Number
83N36060
Funding Number(s)
PROJECT: RTOP 506-63-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available