SEARCH · Search NASA

Results for “ROCKET EXHAUST”

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.

SourceResearch connectionFrom yearThrough year

Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.

At least 253 records · Page 14

All sources NASA NTRS DOE OSTI

NASA NTRS1965

Air-cured ceramic coating insulates against high heat fluxes

Reflective insulating ceramic coating protects supporting structures in area adjacent to rocket engines from the intense heat fluxes in the rocket exhaust plumes.

Seitzinger, V. F.↗

NASA NTRS1966

Study of hot wire techniques in low density flows with high turbulence levels

Prediction of heat, mass, species, and momentum fluxes in a space vehicle and aerodynamic noise production by supersonic jet and rocket exhausts requires a predictability of the associated turbulence fields. The hot wire is a technique that will allow an experimental determination of turbulent properties.

Hanson, A. R.↗

NASA NTRS1966

Investigation of Lunar Surface Chemical Contamination by LEM Descent Engine and Associated Equipment

Lunar surface and atmospheric contamination study caused by LEM rocket exhaust and inorganic, organic, and microbiological contaminants

MICROBIOLOGY↗

NASA NTRS1966

Investigation of lunar surface chemical contamination by LEM descent engine and associated equipment Final report

Lunar surface contamination from LEM rocket exhaust - methods of minimizing sample contamination

LUNAR EXCURSION MODULE /LEM/↗

NASA NTRS1966

Ignition and ignition propagation in solid propellant motors.

Solid propellant ignition and ignition propagation for rocket exhaust and hypergolic-type igniters

CHAMBER PRESSURE↗

NASA NTRS1964

A Heat Transfer Investigation of Ejector Systems with 90 Deg Turns. NERVA Program

Heat transfer characteristics of ejector systems for turning rocket exhaust gases through 90 deg

Mandell, B.↗

NASA NTRS1967

Study of dual channel infrared spectroradiometer systems Interim report

Dual channel infrared spectroradiometer system for obtaining spectral absorption and emission data used to determine temperature and pressure distributions of certain rocket exhaust species

Herget, W. F.↗

NASA NTRS1967

Laboratory simulation of lunar surface erosion by rockets

Laboratory simulation of lunar soil erosion by rocket exhausts

Conner, D. W.↗

NASA NTRS1968

The laser as a meteorological tool.

Meteorogical flowfield velocity and rocket exhaust by-product spectroscopic analysis using laser

Goldstein, I.↗

NASA NTRS1968

A detonation tube technique for simulating rocket plumes in a space environment.

Shock tube simulation of rocket exhaust plumes and effects on vehicles in space environment

Hopkins, H. B.↗

NASA NTRS1969

Propulsion beam divergence effects Quarterly technical report

Experimental equipment for impingement test of electrostatic rocket exhaust jet

Source record↗

NASA NTRS1969

Propulsion beam divergence effects Quarterly technical report

Test equipment, immersion tests, and spectral distribution of solar simulator for studying effects of electrostatic rocket exhaust impingement on spacecraft

Source record↗

NASA NTRS1969

Photometry from Apollo tracking.

Baker-Nunn photometry from Apollo tracking utilizing photographs for brightness, dynamics and duration of rocket exhausts and venting clouds

Lundquist, C. A.↗

NASA NTRS1969

Apollo 11 observations of a remarkable glazing phenomenon on the lunar surface.

Apollo 11 observations of lunar surface glazing, considering radiation heating due to solar outbursts, rocket exhaust effects, shock heating or volcanism, erosion, etc

Gold, T.↗

NASA NTRS1969