NASA NTRS · 19710050067
HTPB propellants for large booster applications
Abstract
Solid propellants based on low cost hydroxyl terminated polybutadiene binders meeting burning rate, mechanical properties and processing requirements for large booster motors
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Bankaitis, H., Smith, P. L.. 1971-06-01. HTPB propellants for large booster applications. https://ntrs.nasa.gov/citations/19710050067
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