Flight-test temperature data for an altair-iic1 rocket motor
Flight test temperature data for Altair IIC1 ROCKET motor
ROCKET ENGINE↗
SEARCH · Engineering Papers
Results for “Motor”
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.
Sterilized solid-propellant rocket motors for mars landing missions revision no. 1
Sterile solid propellant motor for planetary and lunar landings - chemical sterilization, heat sterilizable propellants, and silicone propellant development
SILICONE↗
Design of optimized three-dimensional rocket motor nozzles.
Optimization of supersonic portion of three- dimensional flow geometry in rocket motor nozzle for maximum thrust
THREE-DIMENSIONAL FLOW↗
Ring counter circuit switches multiphase motor direction of rotation
Solid state three-phase counter circuit reverses the direction of rotation of a multiphase motor without changing the phase wiring of the supply current source.
Fairbanks, A. F.↗
Brushless dc motor has high efficiency, long life
Brushless dc motor operates as a commutator in a vacuum environment with high efficiency and long life. Because of its excellent response time, it can be used in the servomechanism field.
Studer, P. A.↗
Fluid logic control circuit operates nutator actuator motor
Fluid logic control circuit operates a pneumatic nutator actuator motor. It has no moving parts and consists of connected fluid interaction devices. The operation of this circuit demonstrates the ability of fluid interaction devices to operate in a complex combination of series and parallel logic sequence.
Source record↗
Scout motor performance analysis and prediction study /PAPS/
Scout motor performance analysis and prediction
SCOUT LAUNCH VEHICLE↗
Aerothermochemical analysis of non-oscillatory and oscillatory characteristics of liquid bipropellant rocket motors - Wave model, droplet heating, and evaporation program computation Third quarterly report no. 65-1
Aerothermochemical analysis of nonoscillatory and oscillatory characteristics of liquid bipropellant rocket motors - wave model, droplet heating, and evaporation computer program
BIPROPELLANT↗
Steady state aerothermochemistry for liquid bipropellant rocket motors
Model and theoretical equations describing liquid propellant droplet ballistics and combustion gas behavior in bipropellant rocket motors - aerothermochemistry
LIQUID PROPELLANT ROCKET ENGINE↗
Evaluation of the Marc 7G1 auxiliary rocket motor for use on the Atlas-Centaur vehicle Final report
Evaluation of Mars 7G1 auxiliary rocket motor for use as retrograde thrust generator on Atlas-Centaur space vehicle
ATLAS CENTAUR LAUNCH VEHICLE↗
Little Joe II Program - Monte Carlo study of motor performance
Monte Carlo method to predict solid propellant variability effects on Algol ID motor performance, for Little Joe II project
LITTLE JOE II LAUNCH VEHICLE↗
Little Joe II Motor Development Program Final report
Algol rocket engine and motor ground support equipment for Little Joe II launch vehicle
ALGOL ROCKET ENGINE↗
A Theoretical Study of Nonlinear Transverse Combustion Instability in Liquid Propellant Rocket Motors
Nonsteady flow conditions in subsonic section of Laval nozzle to investigate nonlinear transverse combustion instability in liquid propellant rocket motors
COMBUSTION INSTABILITY↗
Design study of heat sterilizable solid rocket motors for space application, volume I Final report, Oct. 19, 1965 - Jan. 9, 1966
Design and analysis of heat sterilizable solid propellant rocket motors
SOLID PROPELLANT ROCKET ENGINE↗
Radiative properties of carbon particles produced by a rocket motor.
Radiation from carbon particle clouds produced by research rocket motors
RADIATION MEASUREMENT↗
Applying large solid motors to future launch vehicles.
Solid propellants for future large launch vehicles noting motor configurations, costs, thrust, size, etc
LAUNCH VEHICLE↗
The ignition transient in solid propellant rocket motors.
Ignition pressure transient of rocket motor, discussing initial ignition event, flame spreading and final chamber filling, convective heating effect on burning rate, etc
CONVECTIVE HEAT TRANSFER↗
Hybrid solid state switch replaces motor- driven power switch
Hybrid solid state switch replaces existing motor-driven power switches used on spacecraft. It uses a transistor circuit to limit the open circuit voltage and allow small relay contacts to handle high transient currents at reasonable cycle life.
Booth, R. A.↗