Overstress Qualification Test of the Multiple Satellite Dispenser 0.2 lbf Rocket Engine Assembly REA 10-16.
Standard engineering rept.,
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 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.
- Liquid Propellant Rocket Engines
- Unmanned Spacecraft