NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The European Spacelab structural design evolutionSpacelab is a manned, reusable laboratory which is being developed for the European Space Agency (ESA). In its working mode it will fly in low earth orbit in the cargo bay of the Shuttle Transportation System (STS) Orbiter. A description is presented of the structural development of the various features of Spacelab. System requirements are considered along with structural requirements, quasi-static loads, acoustic loads, pressure loads, crash loads, ground loads, and the fatigue profile. Aspects of thermal environment generation are discussed, and questions regarding the design evolution of the pallet structure are examined. Details of pallet structure testing are reported, taking into account static strength tests, acoustic tests, the modal survey test, crash tests, and fatigue/fracture mechanics testing.
Document ID
19820046585
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Thirkettle, A. J.
(ESA, Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 82-0761
Meeting Information
Meeting: In: Structures, Structural Dynamics and Materials Conference
Location: New Orleans, LA
Start Date: May 10, 1982
End Date: May 12, 1982
Accession Number
82A30120
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available