Analysis Of Guidance Perturbations For A Low-Thrust Mars Orbiter Mission Using Snap-8
Guidance perturbations for a low-thrust mars orbit mission using snap-8
SYSTEM FOR NUCLEAR AUXILIARY POWER-8 /SNAP-8/↗
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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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THRUST AND PUMPING CHARACTERISTICS OF A SERIES OF EJECTORTYPE EXHAUST NOZZLES AT SUBSONIC AND SUPERSONIC FLIGHT SPEEDS
Thrust and pumping characteristics of ejector-type exhaust nozzles at subsonic and supersonic speeds
EJECTOR↗
LOW-TEMPERATURE CHEMICAL STARTING OF A 200-POUND-THRUST JP-4 - NITRIC ACID ROCKET ENGINE USING A THREE-FLUID PROPELLANT VALVE
Low-temperature chemical starting of combined jp-4 nitric acid propellant for low-thrust rocket engine using three-fluid propellant valve
ROCKET ENGINE↗
LARGE-SCALE WIND-TUNNEL TESTS OF A CIRCULAR PLAN-FORM AIRCRAFT WITH A PERIPHERAL JET FOR LIFT, THRUST, AND CONTROL
Wind tunnel tests of circular planform aircraft with peripheral jet for lift, thrust, and control
AIRCRAFT↗
Evaluation of Injector Principles in a 2400-pound-thrust Rocket Engine Using Liquid Oxygen and Liquid Ammonia
Injector evaluation in 2400-pound-thrust rocket engine using liquid oxygen and liquid ammonia
ROCKET ENGINE↗
A Cold-Flow Investigation of Jet-Induced Thrust-Vector Control
Cold-flow performance of thrust-vector control by secondary injection
COLD FLOW TEST↗
THRUST MEASUREMENTS OF COLLOIDAL PARTICLES AS AN INDICATION OF PARTICLE SIZE AND THRUSTOR OPERATION
Measurements of the thrust of a colloidal-particle electrostatic engine and their correlation to thrustor operation
PROPULSION SYSTEM PERFORMANCE↗
OPTIMAL LOW-THRUST NEAR-CIRCULAR ORBITAL TRANSFER
Study of optimum low-thrust transfers between neighboring coplanar circular orbits for a simplified system model
ORBITAL TRANSFER↗
Apparatus measures very small thrusts
Measurement of very small thrusts of an ion engine are made by mounting the engine on a platform supported by leaf springs which are loaded to have a zero spring constant. Measuring apparatus includes an inductive sensor, servo amplifier, and a counterthrust feedback system.
Source record↗
Dynamic pressure and thrust characteristics of cold jets discharging from several exhaust nozzles designed for vtol downwash suppression
Exhaust nozzle testing using cold air flow to find effect of exit design on thrust & jet wake dynamic pressure for use in vtol downwash suppression
DYNAMIC PRESSURE↗
A technique for thrust-vector orientation during manual control of lunar landings from a synchronous orbit
Technique for thrust-vector orientation during manual control of lunar landings from synchronous orbit
MANUAL CONTROL↗
Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.
Payload capabilities of low thrust power limited spacecraft for earth to mars round trip trajectories
ORBITAL TRANSFER↗
The evaluation of a tin-aluminide oxidation resistant coating for reaction control system thrust systems applications final report, 26 jul. 1963 - 1 aug. 1964
Tin-aluminide oxidation resistant coating for reaction control rocket thrust chamber
ALUMINUM COMPOUND↗
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↗
A first order delaunay solution for minimum fuel, low thrust trajectories
First order Delaunay solution for minimum fuel, low thrust trajectories
Passmore, H., III↗
Dynamic stability analysis of a free-free cir- cular cylindrical shell subjected to a gimbaled, periodically-varying end thrust technical memorandum no. 101
Dynamic stability of free-free circular cylindrical shell subjected to gimballed variable end thrust
GIMBALLED CONTROL↗
A describing-function analysis of the stability of a launch vehicle with nonlinear thrust vectoring
Describing-function analysis of launch vehicle stability with nonlinear thrust vectoring
LAUNCH VEHICLE↗
The effect of injector design on thrust- chamber erosion.
Control of injector spray and heat transfer properties can reduce erosion of ablative and pyrolytic graphite thrust-chamber throats
INJECTOR↗