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Consort and Joust sounding rocket missionsThe two suborbital rocket programs are described in terms of their common objective of examining commercial applications of materials processing under microgravitational conditions. The sounding rocket programs have unique launch-service capabilities but provide essentially interchangeable payload accommodations. Major differences include longer low gravity times and larger payload volume for the Joust rocket, spin stabilization and land recovery for the Consort rocket, and faster ascent and reentry accelerations for the Joust rocket. A summary of previous and planned experiments for the rocket programs is given which includes studies of the morphology and strength of elastomer-modified epoxy resins, electrodeposition studies, the demixing of immiscible polymers, foam formation, and polymer experiments. These and other experiments can be facilitated by the microgravity time available on flights of the two sounding rockets.
Document ID
19920030282
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wessling, Francis C.
(Alabama, University Huntsville, United States)
Maybee, George W.
(McDonnell Douglas Space Systems Co. Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Materials Processing
Meeting Information
Meeting: AIAA/IKI Microgravity Science Symposium
Location: Moscow
Country: USSR
Start Date: May 13, 1991
End Date: May 17, 1991
Accession Number
92A12906
Funding Number(s)
CONTRACT_GRANT: NAGW-812
Distribution Limits
Public
Copyright
Other

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