Radiation from carbon in a rocket plume mixing region with coupled convective and radiative energy fluxes and general optical thickness
Carbon radiant heat transfer from plume mixing region to base of rocket vehicle
RADIATIVE HEAT TRANSFER↗
SEARCH · Engineering Papers
Results for “Rocket”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Review of thermal radiation from liquid and solid propellant rocket exhausts
Thermal radiation from liquid and solid propellant rocket exhausts
SOLID PROPELLANT↗
The integrated-circuit control and timing system of the high-altitude rocket-radar project
Integrated circuit control and timing system of high altitude rocket radar
TIMING APPARATUS↗
Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0
Jet-stream interaction effects on rocket engine studied with simulated ballistic missile using liquid oxygen and JP-4 fuel mixture
JP-4 JET FUEL↗
Effects of jet pluming on the static stability of five rocket models at Mach numbers of 4, 5 and 6 and static pressure ratios up to 26,000
Jet pluming effect on static stability of five cone cylinder-flare finned rocket models at Mach numbers of 4, 5, and 6 and static pressure ratios up to 26,000
ROCKET EXHAUST↗
Rocket and satellite studies of meteoric dust
Rocket and satellite measurements on meteoritic dust
METEORITIC DUST↗
Heat and mass-transfer characteristics of an axial-flow liquid-core nuclear rocket employing radiation heat transfer
Heat and mass transfer characteristics of axial- flow liquid-core nuclear rocket engine employing radiation heat transfer
MASS TRANSFER↗
Numerical method for rocket trajectory determination from multistation Doppler tracking data
Numerical method for rocket trajectory determination from multistation Doppler tracking data
POLYSTATION DOPPLER TRACKING SYSTEM↗
Sound ranging computations for sounding rocket recovery
Recovery of reentry rocket by sound ranging detection of shock wave
SHOCK WAVE↗
Axial mode shock wave combustion instability in liquid propellant rocket engines
Axial mode shock wave combustion instability in liquid propellant rocket engines
SHOCK WAVE↗
A compendium of NASA Aerobee sounding rocket launchings for 1966
Compendium of Aerobee sounding rocket launchings for 1964
AEROBEE ROCKET↗
Nonlinear aspects of combustion instability in liquid propellant rocket motors Status report, 1 Jun. 1966 - 31 May 1967
Nonlinear aspects of combustion instability in liquid propellant rocket engines
NONLINEARITY↗
Gaseous-hydrogen liquid-oxygen rocket combustion at supercritical chamber pressures
Chamber pressure variations and rocket combustor performance for gaseous hydrogen-liquid oxygen propellant system
CHAMBER PRESSURE↗
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↗
The integrated rocket spin-up launch mechanism
Integrated rocket spin-up launch mechanism with pyrotechnic and mechanical events initiated by single electric signal
INITIATION↗
Inhomogeneous radiant heat transfer from Saturn rocket exhaust plumes
Inhomogeneous radiant heat transfer from Saturn rocket exhaust plumes
ROCKET EXHAUST↗
Nonlinear combustion instability in liquid-propellant rocket engines. The transverse mode. I. The hydrodynamic differential and difference equations and computer algorithm
Hydrodynamic differential and difference equations and computer algorithm for nonlinear combustion instability in liquid propellant rocket engines, and Fortran IV listing
ALGORITHM↗
Studies related to the development of a multiple start-stop solid propellant rocket motor
Multiple start-stop solid propellant rocket motor using highly aluminized ammonium perchlorate annular propellant grains
SOLID PROPELLANT ROCKET ENGINE↗