Radiation from circumferential slots on plasma-clad cones
Slot antenna radiation pattern distortion produced by boundary layer plasma sheath around conical reentry vehicles
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Slot antenna radiation pattern distortion produced by boundary layer plasma sheath around conical reentry vehicles
Mathematical models predicting reentry plasma effects on admittance, attenuation, isolation, and breakdown characteristics of antenna systems
Low Reynolds number viscous flow at stagnation region of blunt bodies during hypersonic reentry
Electron removal from reentry flow fields by dissociative attachment for blackout alleviation
Reentry plasma sheath alleviation by injecting sulfur hexafluoride or hydrazine into boundary layer
Design of ring wing vehicle of high drag-to-weight ratio to withstand reentry stress into low density atmosphere
Transonic wind tunnel investigation of flow characteristics and pressure fluctuation of space shuttle launch and reentry configurations
Leeside aerodynamic heating of lifting reentry vehicle configurations
Aerodynamic stability control for reentry trajectory of space shuttle orbiter at transition maneuver
Analysis of anomalous jettisoning of service module during reentry of Apollo 11
Analysis of high temperature oxidation rate of carbon for use as reentry material
Techniques and apparatus design for measuring high temperature emissivity of thermal protection materials for reentry vehicles
Space capsule reentry into Martian atmosphere for soft landing, using onboard nonlinear filter and stochastic control for random wind gusts
Space shuttle vibrational characteristics, investigating dynamic models, aeroelasticity, reentry, wing stall flutter and buffet boundaries
Lifting body vehicle handling qualities, considering X-24A, M2-F3 and HL-10 reentry vehicles flight characteristics and simulation requirements
Protective coatings of Ta, Nb and TD alloys for high performance thermal protection systems, discussing space shuttle reentry heat shield
Reentry glider approximate optimal atmospheric entry trajectories for maximizing function of terminal velocity, altitude, flight path and heading angle under terminal nonlinear constraints
Modified perturbation method for solving optimal control boundary value problems with state variable inequality constraints, noting application to reentry trajectories