Program for sea level test firing of rocket engines final report, 1 sep. 1964 - 1 feb. 1965
Bipropellant rocket engines with radiation cooled thrust combustion chambers of molybdenum fired for testing and material evaluation
COMBUSTION CHAMBER↗
SEARCH · Search NASA
Results for “bipropellant”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Surveyor vernier thrust chamber assembly development, phase iii, volumes 1, 2, and appendixes
Surveyor Vernier thrust chamber assembly - bipropellant rocket engine, flow control, control interfaces, and test firing
ROCKET ENGINE↗
An experimental investigation of the effects of combustion on the mixing of highly reactive liquid propellants
Effects of combustion on liquid phase mixing of storable liquid bipropellants
STORABLE PROPELLANT↗
Sterilizable liquid propulsion system Quarterly progress report, 2 Jan. - 31 Mar. 1967
Basic design, component selection, and materials compatibility tests for sterilizable liquid bipropellant propulsion system
PROPULSION SYSTEM↗
Propellant leakage detection system final report
Prototype propellant leakage detection system for bipropellant reaction control systems
DETECTION↗
An experimental correlation of the nonreactive properties of injection schemes and combustion effects in a liquid-propellant rocket engine. Part VI - The relation between the starting transient and injection hydraulics
Gas pressurized, liquid bipropellant injection feed system starting flow transient criteria - effects on combustion stability
FEED SYSTEM↗
Guidance, control, and propulsion systems
In accomplishing the Gemini Program objectives, an onboard digital computer system, an inertial platform reference system, a radar system, and control systems using hypergolic bipropellant propulsion have been developed and successfully demonstrated.
PROPULSION SYSTEM↗
Summary of literature survey of hypergolic ignition spike phenomena, phase I Final report, Apr. 8 - Dec. 31, 1965
Summary of industry survey and literature search of ignition spike phenomena in low thrust, hypergolic, liquid bipropellant rocket engines
HYPERGOLIC PROPELLANT↗
Addition of solid oxidizer increases liquid fuel specific impulse
Adding soluble solid oxidizers to hydrazine and similar fuels makes them useful in low temperature bipropellant systems. These oxidizers improve the low specific impulse, high freezing point, low boiling point, and low density of the fuels.
Hendel, F. J.↗
Report on the development of the Manned Orbital Research Laboratory /MORL/ SYSTEM utilization potential. Task area IV - MORL system improvement study-book 5
Updated bipropellant and advanced thrustor systems for Manned Orbital Research Laboratory, and comparison of integrated propulsion/reaction control systems
PROPULSION SYSTEM↗
Sterilizable liquid propulsion system Quarterly progress report
Module truss, propellant tanks, and functional tests for sterilizable bipropellant liquid propulsion system exposed to ethylene oxide
Brady, H. F.↗
Sterilizable liquid propulsion system Quarterly progress report, Oct. 1 - Dec. 31, 1967
Exposure of assembled and fueled bipropellant liquid rocket propulsion system to ethylene oxide and heat sterilization environments
Brady, H. F.↗
Exploring in aerospace rocketry. 7 - Liquid propellant rocket systems
Operating characteristics and design aspects of injector, combustion chamber, and exhaust nozzle for bipropellant rockets
Conrad, E. W.↗
Sterilizable liquid propulsion system Quarterly progress report, 1 Apr. - 30 Jun. 1967
Hydrazine-based bipropellant liquid propulsion system exposed to ethylene oxide and heat sterilization environments
Brady, H. F.↗
C-1 engine - Propellant valve qualification, volume 2, book 2 Final report
Specifications, design concepts, and qualification test procedures for C-1 engine bipropellant valve
Source record↗
The Apollo Lunar Module Reaction Control System.
Apollo lunar module pressure-fed bipropellant reaction control system design requirements and system description
Grossman, R. L.↗
Sterilizable liquid propulsion system.
Loaded bipropellant liquid propulsion system sterilization studies concerning structural and nonmetallic materials suitability for use in oxidizer
Lukens, S. C.↗
Sterilizable liquid propulsion system Quarterly report, 1 Jan. - 31 Mar. 1969
Fueled bipropellant liquid propulsion system exposed to ethylene oxide and heat sterilization
Lukens, S. C.↗