Accession Number : AD0375465

Title :   FEASIBILITY DEMONSTRATION OF ADVANCED ATTITUDE CONTROL SYSTEMS.

Descriptive Note : Quarterly progress rept. no. 4, 1 May-31 Jul 66,

Corporate Author : BELL AEROSYSTEMS CO BUFFALO N Y

Personal Author(s) : Montanino,L. ; Pearson, W.

Report Date : AUG 1966

Pagination or Media Count : 25

Abstract : The period was devoted to accomplishing the following work for Task 1 - Completion of testing of the single coaxial injector configuration fabrication, assembly and testing of the multiple coaxial injector configuration and selection for thrust chamber durability testing, modification of one bipropellant valve to eliminate a flow choking condition, and preparation of the tungsten coated thrust chamber for welding to the multiple coaxial injector. Task 2 - Leak and gas volume checks of the fuel and oxidizer bellows pumps, assembly completion of the second heat exchanger, completion of the test setup for injector checkout tests, and initiation of injector tests with the single coaxial injector.

Descriptors :   (*ATTITUDE CONTROL SYSTEMS, *LIQUID PROPELLANT ROCKET ENGINES), RESEARCH MANAGEMENT, INJECTORS, FUEL INJECTORS, CONSTRUCTION, ASSEMBLY, MODIFICATION KITS, PROPELLANT CONTROL, VALVES, TUNGSTEN, METAL COATINGS, COMBUSTION CHAMBERS, BELLOWS, LEAKAGE(FLUID), FEASIBILITY STUDIES, VOLUME, HEAT EXCHANGERS, TEST EQUIPMENT (U) CONTROL JETS, GASEOUS ROCKET PROPELLANTS, FLUORINE, HYDROGEN, IGNITION, FUEL ADDITIVES, OXYGEN COMPOUNDS, FLUORIDES, METHANE

Subject Categories : Liquid Propellant Rocket Engines
      Unmanned Spacecraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE