The report presents the results of a Qualification Test Program on Hamilton Standard Rocket Engine Assembly Model 10-16, a nominal 0.2 pound thrust monopropellant engine. The purpose of this test program was to demonstrate that this engine meets the performance and environmental requirements of the Naval Research Laboratories specification, NRL RFP N00014-73-R-0011, Part 2.
Qualification Test for the Multiple Satellite Dispenser 0.2 LBF, Rocket Engine Assembly REA 10-16
1973
318 pages
Report
No indication
English