SCALING PROBLEMS ASSOCIATED WITH UNSTABLE BURNING IN SOLID PROPELLANT ROCKETS
Scaling in unstable combustion processes of solid propellant rocket engines
SOLID PROPELLANT ROCKET ENGINE↗
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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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Free-Flight Investigation of Aerodynamic Heat Transfer to a Simulated Glide-Rocket Shape at Mach Numbers up to 10
Heat-transfer measurements were made on a simulated glide-rocket shape in free flight at Mach numbers up to 10 and free-stream Reynolds numbers of 2 x 10 based on distance along surface from apex and 3 x 10 based on nominal leading-edge diameter. The model simulated the bottom of a 75 deg delta wing at 8O deg angle of attack. The data indicated that for the test conditions a modified three-dimensional stagnation-point theory will predict to reasonable engineering accuracy the heating on a highly swept wing leading edge, the heating being reduced by sweep by the 3/2 power of the cosine of the sweep angle. The data also indicate that laminar heating rates over the windward surface of a highly swept flat glider wing at moderate angles of attack can be predicted with reasonable engineering accuracy by flat-plate theory using wedge local flow conditions and basing Reynolds numbers on lengths from the wing leading edge parallel to the surface center line.
FREE FLIGHT↗
SPACE-SIMULATED TESTING OF MARINER SPACECRAFT AUTOPILOT SYSTEMS WITH ROCKET MOTOR FIRING
Space simulator test of mariner spacecraft autopilot systems with rocket motor firing
SPACE SIMULATOR↗
AN EXPERIMENTAL INVESTIGATION OF GASEOUS-FILM COOLING OF A ROCKET MOTOR
Gaseous-film cooling of rocket combustion chamber
GAS COOLING SYSTEM↗
A GENERAL IBM 704 OR 7090 COMPUTER PROGRAM FOR COMPUTATION OF CHEMICAL EQUILIBRIUM COMPOSITIONS, ROCKET PERFORMANCE, AND CHAPMAN-JOUGUET DETONATIONS. SUPPLEMENT I - ASSIGNED AREA-RATIO PERFORMANCE
Computer program for computation of chemical equilibrium compositions, rocket performance, and chapman-jouguet detonations
COMPUTER PROGRAM↗
METHODS FOR INFRA-RED ANALYSIS OF ROCKET FLAMES IN SITU
Methods for infrared analysis of rocket flames in situ
INFRARED SPECTROSCOPY↗
NUCLEAR-ROCKET APPLICATIONS
Examination of possible space applications of nuclear rockets, considering only solid-core reactors
MANNED SPACECRAFT↗
COST-OPTIMIZING MULTISTAGE ROCKETS
Cost-optimization method for the selection of the booster system and its optimum rocket sizes, based on the economics of achieving the mission
MULTISTAGE ROCKET VEHICLE↗
DESIGN, DEVELOPMENT AND OPERATION OF LIQUID ROCKET VEHICLES
Significance of the performance factors, specific impulse and vehicle mass ratio of liquid propelled rockets, so as to produce maximum capability
SPACECRAFT DESIGN↗
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↗
EVALUATION OF A CESIUM-ION ROCKET EMPLOYING A LARGE POROUS TUNGSTEN IONIZER
Evaluation of a cesium-ion rocket engine employing a large porous tungsten ionizer
ION ENGINE↗
SINGULAR EXTREMALS IN LAWDEN'S PROBLEM OF OPTIMAL ROCKET FLIGHT
Derivation of the singular extremals of lawdens problem of optimal rocket flight by use of the legendre-clebsch necessary condition applied in a transformed system of state and control variables
EULER-LAGRANGE EQUATION↗
SOME ASPECTS OF STRATOSPHERIC CIRCULATION DERIVED FROM METEOROLOGICAL ROCKET FIRINGS OVER THE UNITED STATES DURING THE WINTER OF 1961
Wind and temperature data from meteorological rocket firings over the united states during the winter of 1961 and the relationship of the polar vortex
ATMOSPHERIC CIRCULATION↗
SINGULAR EXTREMALS IN LAWDEN'S PROBLEM OF OPTIMAL ROCKET FLIGHT
Optimal rocket flight in gravitational field using lawdens results on intermediate thrust subarcs
ROCKET FLIGHT↗
ROCKET AND SATELLITE INVESTIGATIONS OF THE IONOSPHERE
Rocket and satellite measurements of the d-region under quiet and disturbed solar conditions, ionospheric ion and electron density, and electron temperatures
ROCKET SOUNDING↗