The report presents the results of a portion of a qualification overstress test on Hamilton Standard Rocket Engine Assembly 10-16, a nominal 0.2 footpounds thrust hydrazine monopropellant engine. This phase of the testing was concerned with verification of nozzle thrust coefficients and critical soakback testing of the REA.
Overstress Qualification Test of the Multiple Satellite Dispenser 0.2 lbf Rocket Engine Assembly REA 10-16
1973
41 pages
Report
No indication
English
Hyperstaticity in Satellite Dispenser Design, Justification and Qualification
British Library Conference Proceedings | 2001
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