A total of forty-one injector development test firings were made using eight injector configurations. Three chamber lengths were evaluated with a single injector configuration. Satisfactory performance was achieved with the longest chamber tested. Injector dynamic stability was demonstrated in numerous stability rating tests. Three demonstration injectors were designed and fabricated and two of these injectors were subjected to checkout firings.
Injector/Chamber Scaling Feasibility Program. Volume 1. Design and Short Duration Testing
1970
279 pages
Report
No indication
English
Rocket Engines & Motors , Combustion & Ignition , Liquid propellant rocket engines , Fuel injectors , Combustion chambers , Fuel injection , Feasibility studies , Captive tests , Thrust , Configuration , Stability , Ablation , Combustion , Design , Model tests , Costs , Thermal analysis , Scaling , Pintles , Nitrogen compounds , Tetroxides , Coaxial fuel injectors , Ablative materials
Injector/Chamber Scaling Evaluation
NTIS | 1972
|Injector/Chamber Scaling Evaluation, Facility Checkout
NTIS | 1969
|The effect of injector design on thrust- chamber erosion
AIAA | 1965
|The Effect of Injector Design on Thrust- Chamber Erosion
NTIS | 1966
|