The report presents the results of a portion of a Qualification Overstress Test on Hamilton Standard Rocket Engine Assembly, Model 16-9, a nominal 5.0 pound thrust monopropellant engine. The objectives of this portion of the Qualification Overstress Tests were to characterize the engine over extended life and at various operating conditions.
Overstress Qualification Test of the Multiple Satellite Dispenser 5 LBF Rocket Engine Assembly REA 16-9
1973
196 pages
Report
Keine Angabe
Englisch
Hyperstaticity in Satellite Dispenser Design, Justification and Qualification
British Library Conference Proceedings | 2001
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