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HTPB propellants for large booster applicationsSolid propellants based on low cost hydroxyl terminated polybutadiene binders meeting burning rate, mechanical properties and processing requirements for large booster motors
Document ID
19710050067
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bankaitis, H.
Smith, P. L.
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propellants
Report/Patent Number
AIAA PAPER 71-708
Report Number: AIAA PAPER 71-708
Meeting Information
Meeting: PROPULSION JOINT SPECIALIST CONFERENCE
Location: SALT LAKE CITY, UT
Country: US
Start Date: June 14, 1971
End Date: June 18, 1971
Sponsors: SOCIETY OF AUTOMOTIVE ENGINEERS, AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A30764
Distribution Limits
Public
Copyright
Other

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