A design study of a regeneratively cooled nozzle for a tungsten water-moderated nuclear rocket system
Regeneratively cooled nozzle for tungsten water moderated nuclear rocket system
ROCKET NOZZLE↗
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Results for “rockets”
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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RL10A-3-3 rocket engine Design report
Design features of RL-10 A-3 liquid propellant rocket engine
RL-10 A-3 ROCKET ENGINE↗
A compendium of NASA Aerobee sounding rocket launchings for 1964
Overall Aerobee sounding rocket flight performance for 1964 launchings
AEROBEE ROCKET↗
An evaluation of an operational sounding rocket to fulfill a new 100 kilometer requirement
Analysis of flight characteristics and static stability of Tomahawk vehicle for use with 100-kilometer sounding rocket
NIKE-TOMAHAWK ROCKET↗
Nose selection and vehicle motion dynamics for the second stage of a two-stage sounding rocket system
Nose selection and vehicle motion dynamics for Nike-Tomahawk rocket
NIKE-TOMAHAWK ROCKET↗
Investigation of a submerged nozzle for solid rockets
Scale model compressed air tests of 260-inch solid rocket with submerged nozzle to determine exhaust flow velocity and direction in annular channel
ANNULAR FLOW↗
Cooldown characteristics of regenerative nozzle used in full-scale, cold-flow, nuclear rocket test facility
Transient pressure drop and heat transfer characteristics of regeneratively cooled nozzle assembly used in full scale, cold flow nuclear rocket test facility
REGENERATIVE COOLING↗
Grounding of rocket experiments
Experiment design and construction for rocket engine noise protection, and grounding of amplifier circuit
ELECTRIC GROUNDING↗
Feasibility, parametric design, and comparative analysis of an unguided solid fuel rocket vehicle with solar orbit, earth probe, and re-entry mission capabilities
Feasibility, parametric design, and comparative analysis of unguided solid fuel rocket vehicle with solar orbit, earth probe, and reentry mission capabilities
STRUCTURAL DESIGN↗
Static stability investigation of a single- stage sounding rocket at Mach numbers from 0.60 to 1.20
Static stability of single-stage meteorological sounding rocket at Mach numbers from 6.0 to 12.0
STATIC STABILITY↗
Results of a Sounding Rocket experiment to study celestial X-ray sources Final report
Sounding rocket experiment to study celestial X-ray sources
CRAB NEBULA↗
Physical parameters of cosmic dust obtained from rocket collections
Cosmic dust particle properties obtained from Aerobee rocket measurements
PARTICLE PROPERTY↗
Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure
Heat-transfer rates and coefficients and coolant pressure loss characteristics in regeneratively cooled liquid hydrogen-liquid fluorine rocket engine thrust chambers
PRESSURE DROP↗
Activation and Initial Test Operations, Large Rocket Engine - Thrust Chamber Test Facilities Technology Report
Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engine
ROCKET TEST STATION↗
An evaluation of an operational sounding rocket to fulfill a new 100 kilometer requirement.
Payload-apogee altitude performance, static stability and dynamic motions of Tomahawk vehicle analyzed for ability to meet 100 km sounding rocket requirement
STATIC STABILITY↗
Development of the Aerobee 350 sounding rocket.
Aerobee 350 sounding rocket for scientific use in heavy payload to moderate altitude performance region
PROPULSION SYSTEM PERFORMANCE↗
Recent developments in neutralization of meteorological rocket falling mass hazards.
Sounding rocket disintegration studies to avoid falling mass hazards, noting design of pyrotechnic core in sandwich construction
SOUNDING ROCKET↗
A Gyroless Solar Pointing Attitude Control System for the Aerobee Sounding Rocket
Gyroless Solar Pointing Aerobee Rocket Control System /SPARCS/ using no inertial platform and having solid state circuitry
ATTITUDE CONTROL↗