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↗
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Results for “Solid Rocket Engine”
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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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↗
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↗
A method for obtaining temperature profiles for solid propellant motor exhaust streams.
Theoretical analysis of heat transfer in solid propellant rocket exhaust plumes by use of temperature probe located in plume environment
SOLID PROPELLANT ROCKET ENGINE↗
Saturn auxiliary solid propulsion applications.
Auxiliary solid propellant motors in Saturn launch vehicle
SATURN LAUNCH VEHICLE↗
Solid boost thrust decay control for stage separation.
Solid booster thrust decay control for payload or upper stage separation, noting inert slivers with auxiliary retrorockets as separation control
THRUST CONTROL↗
Analysis and prediction of effects of exhaust products from aluminized solid-propellant rocket motors on launch facilities.
Effect on protective coatings of launch pads of exhaust products, chamber pressure, nozzle diameter, etc, from aluminized solid propellant rocket motors
PROTECTIVE COATING↗
Heat sterilizable solid propellant motor designs for interplanetary missions.
Heat sterilizable solid propellant motor designs for interplanetary missions, considering case- bonded spherical, case-bonded cylindrical, free- standing, internal burning and free-standing end burning
SOLID PROPELLANT ROCKET ENGINE↗
The ignition transient in solid propellant rocket motors.
Ignition pressure transient in solid rocket motors, examining chamber filling interval, flame propagation, heat transfer correlation, burning area, etc
TRANSIENT PRESSURE↗
On the dynamic characteristics of a variable- mass slender elastic body under high accelerations.
Dynamic characteristics of variable mass slender elastic body, solving vector differential equations
VARIABLE MASS SYSTEM↗
Advanced propulsion applications to new sounding rocket design.
Solid and hybrid propulsion relationship to sounding rocket vehicle design and mission analysis, particularly application to synoptic meteorology
SOUNDING ROCKET↗
Feasibility and Design Study of an Unguided Solar Orbital Launch Vehicle
Feasibility and design study of unguided solar orbital launch vehicle
LAUNCH VEHICLE CONFIGURATION↗
Optimization of base thermal protection system for advanced Saturn II boosters employing strap-on solid propellant motors.
Optimization of base thermal protection system for advanced Saturn II boosters employing strap-on solid propellant motors
THERMAL RADIATION↗
Investigation of a submerged nozzle for solid rockets.
Submerged nozzle for solid rockets, noting exhaust flow velocity and direction determination
EXHAUST VELOCITY↗
Effects of exhausts from aluminized solid propellants on launch facilities.
Effect on protective coatings of launch pads of exhaust products, chamber pressure, nozzle diameter, etc, from aluminized solid propellant rocket motors
PROTECTIVE COATING↗
On the dynamic characteristics of a variable- mass slender elastic body under high accelerations.
Dynamic characteristics of variable mass slender elastic body, solving vector differential equations
SOLID PROPELLANT ROCKET ENGINE↗
Remote size measurements of particulate products of heterogeneous combustion.
Rocket chamber pressure influence on particle size measurements of heterogeneous combustion products of solid propellants containing aluminum
COMBUSTION PRODUCT↗
Optimization of base thermal protection system for advanced Saturn II boosters employing strap-on solid-propellant motors.
Optimization of base thermal protection system for advanced Saturn II boosters employing strap-on solid propellant motors
SOLID PROPELLANT ROCKET ENGINE↗