Cinefluorography of small ablative thrust chambers during hot firing.
X-ray image intensifier in conjunction with motion picture film sequencing of thrust chamber image during hot firing to obtain failure analysis data
CINEFLUOROGRAPHY↗
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Results for “THRUST”
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.
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Optimal free-space fixed-thrust trajectories using impulsive trajectories as starting iteratives.
Optimal free-space fixed thrust trajectories using impulsive trajectories as starting iteratives
TRAJECTORY OPTIMIZATION↗
Application of a finite-difference Newton- Raphson algorithm to problems of low-thrust trajectory optimization.
Low thrust trajectory optimization, using Newton- Raphson method to solve nonlinear two-point boundary value problem
TRAJECTORY OPTIMIZATION↗
Experimental performance of a low-thrust, divergent-flow, Contact-ionization electrostatic thrustor.
Low thrust divergent flow cesium-on-tungsten contact ionization electrostatic thrustor for satellite attitude control and stationkeeping missions
ION ENGINE↗
Computer experiments on ion beam deflection for thrust vector control.
Digital computer program for solution of space- charge-flow problem applied to design of thrustors with variable thrust vector, analyzing two ion- thrustor configurations with aid of computer
COMPUTER PROGRAM↗
A manual method for control of the thrust axis during planar ascent from the lunar surface to a circular orbit
Simple control reference as aid to thrust axis orientation during ascent of lunar module from lunar surface to circular orbit and rendezvous with command and service module
LUNAR ORBITAL RENDEZVOUS /LOR/↗
Jupiter high-thrust round-trip trajectories
Propulsion requirement for high-thrust round-trip trajectories to Jupiter
ROUND-TRIP TRAJECTORY↗
Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
DYNAMIC PROGRAMMING↗
A Two-Variable Asymptotic Solution for Three - Dimensional, Solar-Powered, Low-Thrust Trajectories in the Vicinity of the Ecliptic Plane
Two-variable asymptotic solution for three-dimensional solar powered low thrust trajectories in vicinity of ecliptic plane
ELECTRIC PROPULSION↗
Experimental evaluation of six ablative-material thrust chambers as components of storable-propellant rocket engines
Test firing evaluation of six ablative-material thrust chambers as components of storable propellant rocket engines
COMBUSTION CHAMBER↗
Activation and Initial Test Operations, Large Rocket Engine - Thrust Chamber Test Facilities Technology Report
Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engine
ROCKET TEST STATION↗
Precision flow measurement techniques for low thrust auxiliary propulsion liquid rockets
Precision flow measurement techniques for low thrust auxiliary propulsion liquid rockets
FLOW MEASUREMENT↗
The effect of several injector face baffle configurations on screech in a 20,000-pound thrust hydrogen-oxygen rocket.
Effect of several injector face baffle configurations on screech in 20,000-lb thrust hydrogen-oxygen rocket
HYDROGEN OXYGEN /HOPE/ SPACECRAFT↗
Low-thrust propulsion for the MORL.
Advanced low thrust propulsion systems and propellants evaluation for stationkeeping and stability control of NASA Manned Orbital Research Laboratory
STABILITY AND CONTROL↗
Quasilinearization determination of optimum finite-thrust orbital transfers.
Quasi-linearization determination of optimum finite thrust and impulsive orbital transfers
TRAJECTORY OPTIMIZATION↗
Experimental performance of a low-thrust, divergent-flow, contact-ionization electrostatic thruster.
Low thrust divergent flow cesium-on-tungsten contact ionization electrostatic thrustor for satellite attitude control and stationkeeping missions
SATELLITE ATTITUDE CONTROL↗
Determination of the attitude of a spinning rocket under thrust with statistically varied inputs.
Motion equations of spin-stabilized rocket under thrust with jet damping, variable mass and momentum effects and all angular disturbances
ANGULAR MOTION↗
Optimal and suboptimal guidance and control for low thrust orbital transfer.
Suboptimal feedback solution to guidance and control in minimum time and fuel for low thrust orbital transfer
OPTIMAL CONTROL↗