OPTIMUM EARTH-TO-MARS ROUNDTRIP TRAJECTORIES UTILIZING A LOW-THRUST POWER-LIMITED PROPULSION SYSTEM
Payload capabilities of vehicle containing low- thrust power-limited propulsion system for earth- to-mars roundtrip mission
PAYLOAD↗
SEARCH · Engineering Papers
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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EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER RATES IN ROCKET THRUST CHAMBERS
Analysis of heat transfer in rocket engine thrust chambers that use convergent-divergent nozzles
ROCKET ENGINE↗
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
Regenerative and radiation cooling, transpiration or film cooling, ablation and inert or endothermic heat sink, used in selecting optimum spacecraft engine thrust chamber cooling techniques
ENGINE COOLANT↗
Thrust measurements of colloidal particles as an indication of particle size and thrustor operation
Thrust measurements of colloidal particles as indication of particle size & thrustor operation
THRUSTOR↗
Constants of the motion for optimum thrust trajectories in a central force field
Constants of motion for optimum thrust trajectories in central force field
OPTIMUM THRUST PROGRAMMING↗
Perturbation solutions for low thrust rocket trajectories
Perturbation solutions for equations of motion of vehicle subjected to low thrust acceleration
MOTION EQUATION↗
Spacecraft engine thrust chamber cooling final report, 13 may 1963 - 12 apr. 1964
Cooling thrust chamber of liquid propellant rocket engine using pyrolytic graphite and hydrocarbon film
PYROLYTIC GRAPHITE↗
Some requirements of electric and chemical thrust systems for space station drag cancel- lation
Electrical and chemical thrust devices for application to atmospheric drag cancellation on space station configuration
THRUST↗
Experimental studies on lateral thrust components in solid fuel propulsion units <experimentelle untersuchungen uber querschubkomponenten bei feststofftriebwerken<
Lateral force experiment studies on thrust control of solid fuel propulsion rockets
SOLID PROPELLANT ROCKET ENGINE↗
A radial, diaphragm-separated injection method for variable thrust liquid rocket engines with or without mixture ratio variation <eine radiale, membrangetrennte einspritzmethode fur flussigkeitsraketentriebwerke mit variablem schub und/oder variable
Radial, diaphragm separated injection method for variable thrust liquid rocket engines with or without mixture ratio variation
VARIABLE THRUST↗
Errors Associated with Spinning-up and Thrusting Symmetric Rigid Bodies
Errors associated with spinning-up and thrusting symmetric rigid bodies
RIGID BODY↗
Analysis of the hydrostatic journal and thrust gas bearing for the nasa ab-5 gyro gimbal bearing
Hydrostatic pressurized gas lubricated journal and thrust bearings for gyroscope gimbal bearings - static and dynamic load and flow analysis
GAS LUBRICATED BEARING↗
Parametric study of lunar landing techniques using a predetermined thrust orientation
Parametric study of variation in trajectory parameters for predetermined thrust orientation angle to perform lunar descent from parking orbit
LUNAR ORBIT↗
Optimum correction of thrust transient measurements
Optimum correction of distorted thrust transient measurements
DISTORTION↗
Calculations of mass-flow and thrust produced for a two-phase fluid mixture passing through a choked nozzle
Calculation of mass-flow and thrust produced for two-phase fluid mixture passing through choked nozzle
MASS FLOW↗
Optinal variable-thrust rendezvous of a power- limited rocket between neighboring low- eccentricity orbits final report
Optimal variable thrust rendezvous of power limited rocket between neighboring low eccentricity orbits
ECCENTRICITY↗
Some numerical results of geocentric low thrust trajectory optimization
Determination of optimum, coplanar, circle-to- circle, transfer trajectories for low thrust space vehicles in strong central force field
TRAJECTORY ANALYSIS↗
Experimental performance of gaseous hydrogen and liquid oxygen in uncooled 20,000-pound-thrust rocket engines
Gaseous hydrogen and liquid oxygen experiments in uncooled 20,000-pound-thrust rocket engines
HYDROGEN↗