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GASCan 2 payload integrationThis project, conducted in cooperation with the NASA Advanced Space Design Program, is part of an ongoing effort to place an experiment package into space. The goal of this project is to build and test flight-ready hardware that can be launched from the Space Shuttle. Get Away Special Canister 2 (GASCan 2) consists of three separate experiments. The Ionospheric Properties and Propagation Experiment (IPPE) determines effects of the ionosphere on radio wave propagation. The Microgravity Ignition experiment (MGI) tests the effects of combustion in a microgravity environment. The Rotational Fluid Flow experiment (RFF) examines fluid behavior under varying levels of gravity. This year the following tasks were completed: design of the IPPE antenna, X- and J-cell battery boxes, J-cell battery box enclosure, and structural bumpers; construction of the MGI canisters, MGI mounting brackets, IPPE antenna, and battery boxes; and the selection of the RFF's operating fluid and the analysis of the fluid behavior under microgravity test conditions.
Document ID
19960000875
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Cody, Dennis J.
(Worcester Polytechnic Inst. MA, United States)
Concepcion, Allan G.
(Worcester Polytechnic Inst. MA, United States)
Watras, Edward C., III
(Worcester Polytechnic Inst. MA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Subject Category
Astronautics (General)
Report/Patent Number
NAS 1.26:199447
NASA-CR-199447
Report Number: NAS 1.26:199447
Report Number: NASA-CR-199447
Accession Number
96N10875
Funding Number(s)
PROJECT: PROJ. ME-HJ-9402
CONTRACT_GRANT: NAGW-4290
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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