Rocket exhaust effects on radio frequency transmission.
RF transmission through plasmas created by rocket exhaust of Saturn vehicle
SATURN LAUNCH VEHICLE↗
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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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Exhaust measurements on the plasma from a pulsed coaxial gun.
Ion density and velocity in nitrogen exhaust plasma from pulsed coaxial gun on basis of current measurements
ION DENSITY↗
Analysis of the turbulent mixing between a reactive gas-particle rocket exhaust and a confined airstream.
Air-augmented rocket engine performance prediction requires detailed study of mixing region between reactive gas-particle rocket exhaust and confined airstream
THRUST AUGMENTATION↗
Exhaust jet wake and thrust characteristics of several nozzles designed for VTOL DOWNWASH suppression. Tests in and out of ground effect with 70 deg F and 1200 deg F nozzle discharge temperatures
Jet wake degradation and thrust characteristics of exhaust nozzles designed for VTOL downwash suppression and fuselage and ground effects
EXHAUST NOZZLE↗
An investigation of highly underexpanded exhaust plumes impinging upon a perpendicular flat surface
Underexpanded rocket nozzle exhaust plumes impinging upon perpendicular flat surface
ROCKET NOZZLE↗
Contribution of combustion noise to overall rocket exhaust jet noise
Low frequency noise measurements of Saturn rocket engine, and combustion noise contribution to overall rocket exhaust jet noise
NOISE MEASUREMENT↗
Calculation of axisymmetric exhaust nozzles with an allowance for equilibrium physicochemical reactions
Axisymmetric exhaust nozzle calculations with allowance for physicochemical reactions
PHYSICAL CHEMISTRY↗
Design Handbook for Protection of Launch Complexes from Solid Propellant Exhaust
Design handbook for protection of launch complex from solid propellant exhaust
PROTECTION↗
Solid-Propellant Rocket Exhaust Effects /SPREE/ and methods of attenuation, volume I - Project summary
Solid propellant rocket exhaust effects and methods of attenuation - project summary
SOLID PROPELLANT ROCKET ENGINE↗
Velocity profiles and eddy viscosity distributions downstream of a Mach 2.22 nozzle exhausting to quiescent air
Compressible, turbulent, axisymmetric mixing for velocity profiles and eddy viscosity distributions downstream of Mach 2.2 nozzle exhausting to quiescent air
EXHAUST NOZZLE↗
Experimental analysis of the exhaust beam from a colloid thrustor.
Exhaust beam from colloid thrustor investigated, using quadrupole mass filter
EXHAUST JET↗
Radio propagation effects of rocket exhaust plasmas.
Rocket exhaust plasma disturbance on radio transmission between vehicle and ground station noting multipath, forward and backscatter
PLASMA-ELECTROMAGNETIC INTERACTION↗
Rocket exhaust effects on radio frequency transmission.
RF transmission through plasmas created by rocket exhaust of Saturn vehicle
RADIO TRANSMISSION↗
A short-duration technique for simulated rocket exhaust and wind tunnel flow and its application to the study of scale effect of recirculating flow fields.
Short duration simulation of rocket exhaust products, flow duration through nozzle and effect on recirculation flow fields
FLOW FIELD↗
Effect of rocket exhausts on infrared planet sensors.
Propellant rocket exhaust plume effect on error calculation for radiation balance IR tracker
HORIZON SENSING↗
An inviscid analysis of the plume created by multiple rocket engines and a comparison with available Schlieren data. I - Calculation of multiple rocket engine exhaust plumes by the method of characteristics. II - A finite difference method.
Multiple rocket engine exhaust plumes calculated by method of characteristics and finite difference and compared with schlieren data
ROCKET EXHAUST↗
Effects of exhaust plasmas upon signal transmission to and from rocket powered vehicles.
Signal transmission disturbances caused by presence of rocket exhaust plasmas in propagation medium between ground station and rocket powered vehicle
SIGNAL TRANSMISSION↗
Secondary flow rates in a vertical diffuser of decreasing length using a rocket exhaust jet as the motive fluid
Secondary water flow rates in vertical diffuser of decreasing length using rocket exhaust jet as motive fluid - model sound compressor
WATER FLOW↗