Payload carrier systems for conducting sortie mode scienceThe capabilities and characteristics of the payload carriers developed to provide structural and operational interfaces between the Space Shuttle and the various types of experiments designed to operate in the sortie mode are discussed. The Spacelab is a flexible laboratory system composed of interchangeable elements that can be put together in eight different combinations of pallets and pressurized modules, and provides considerable standard services to users in such areas as equipment installation, power distribution, thermal control, command and data management, software, pointing systems and crew participation. A modular three-axis pointing control system designated the Annular Suspension and Pointing System, is being developed to provide additional pointing capabilities to those payloads that require capabilities not provided by the Spacelab instrument pointing system. Two engineering models of the Spacelab pallet have been designated Orbital Flight Test Pallets which, together with a special experiment support structure, are intended for initial and operational payloads that do not constitute a complete Spacelab mission. The simplest and smallest payload carriers are the Getaway Special cans, intended for small, self-contained, self-sufficient payloads, and the orbiter middeck lockers. In this way, most of the user requirements for Shuttle sortie missions identified to date can be fulfilled.
Document ID
19810036311
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jean, O. C. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Allen, L. B. (NASA Marshall Space Flight Center Spacelab Payload Projects Office, Huntsville, Ala., United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 81-0269Report Number: AIAA PAPER 81-0269
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: St. Louis, MO
Start Date: January 12, 1981
End Date: January 15, 1981
Sponsors: American Institute of Aeronautics and Astronautics