Overstress Qualification Test of the Multiple Satellite Dispenser 5 LBF Rocket Engine Assembly REA 16-9,

摘要

The report presents the results of a portion of a Qualification Overstress Test on Hamilton Standard Rocket Engine Assembly,Model 16-9, a nominal 5.0pound 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.