Overstress Qualification Test of the Multiple Satellite Dispenser 0.2 LBF Rocket Engine Assembly, REA 10-16.
HAMILTON STANDARD WINDSOR LOCKS CONN
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The report presents the results of a portion of a Qualification Overstress Test on Hamilton Standard Rocket Engine Assembly, Model 16-10, a nominal 0.2 pound thrust monopropellant engine. The purpose of the tests performed was to establish engine characteristics over extended life and to establish performance parameters over a range of operating conditions.
- Liquid Propellant Rocket Engines
- Unmanned Spacecraft