This report describes the results of the checkout test series conducted at the High Thrust Facility. This project, a task under the overall Minimum Cost Design Launch Vehicle Program, will develop low-cost high-performing injectors at 250,000 pounds thrust using N2O4/UDMH propellants and will evaluate their scalability up to the multimillion-pound-thrust class.
Injector/Chamber Scaling Evaluation, Facility Checkout
1969
74 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Combustion & Ignition , Rocket Propellants , Manufacturing Processes & Materials Handling , Fuel injectors , Liquid propellant rocket engines , Combustion chambers , Thrust , Liquefied gases , Liquid rocket propellants , Cost effectiveness , Hydrogen , Cryogenics , Instrumentation , Liquid rocket oxidizers , Fluid flow , Thermochemistry , Thermal properties , Propellant tanks
Injector/Chamber Scaling Evaluation
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