Role of mixing in the chemical oxygen-iodine laser reactions
Role of fuel chemical properties on combustor radiative heat load
Review of Evaluation Methodologies for Satellite Exterior Materials in Low Earth Orbit
Responsiveness in Low Orbits Using Electric Propulsion
Responsive Maneuver Planning for Sun-Synchronous Repeating Ground Track Orbits
This paper investigates the suitability of sun-synchronous orbits (SSOs) as an injection location for responsive, maneuverable
...Response of Premixed Stoichiometric Oxy Flames to Strain: Role of Chemistry and Transport
Requirements Analysis of Propulsion Systems for Lunar-Exploration Mission
Reduced Chemical Kinetic Mechanisms for Hydrocarbon Fuels
Real-Gas Effects for Shock/Shock Interaction in Earth and Mars Atmospheres
Shock/shock interactions of types IV, V, and VI are simulated for Earth and Mars conditions using perfect-gas, real-gas chemical
...Reactivity and Hypergolicity of Solid Fuels with Mixed Oxides of Nitrogen
This paper reports on the reactivity and hypergolicity of different solid fuels with both nitrogen tetroxide (NTO) and mixed oxides of
...Reaction Rates for Hypergolic Propellants Using Chemical Delay Times
Reaction Control Thruster Thermal Design for a Mission to Mercury
This paper describes two novel methods used to reduce the prefiring injector temperatures of thrusters on the sun-facing side of a
...Rate-Controlled Constrained Equilibrium for Nozzle and Shock Flows
The performance of different constraints for the rate-controlled constrained-equilibrium (RCCE) method is investigated in the context of
...Rapid Evaluation of Low-Thrust Transfers from Elliptical Orbits to Geostationary Orbit
Low-thrust orbit transfers to geostationary equatorial orbit (GEO) will likely use a combination of chemical and electrical propulsion
...Ram accelerator - A new chemical method for accelerating projectilesto ultrahigh velocities
Radio-Frequency Ion Thrusters—Power Measurement and Power Distribution Modeling
Radiative Heat Transfer in Solid Rocket Nozzles
Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors
Surface roughness and radiation effects on the erosion behavior of a graphite nozzle are studied for both metallized and nonmetallized
...Quasi-One-Dimensional Model of Scramjet Combustor Coupled with Regenerative Cooling
Quasi-0D-Model Mapping of Reflected Shock Tunnel Operating Conditions