Optimization of three-dimensional reentry trajectories.
Optimal control for minimization of heating and acceleration forces to reduce kinetic energy of reentry vehicle in space missions
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Optimal control for minimization of heating and acceleration forces to reduce kinetic energy of reentry vehicle in space missions
Apollo type reentry trajectory optimization numerical methods
Numerical optimization of atmospheric reentry trajectories by sweep method
Radio blackout alleviation and plasma diagnostic results from 25000 foot per second blunt body reentry
Low subsonic aerodynamic characteristics of medium hypersonic L/D reentry spacecraft configuration with variable geometry wing
Transonic aerodynamic characteristics of variable geometry reentry vehicle with hypersonic lift drag ratio
Thermal property requirements of reentry protection on isotope heat sources
Integral launch and reentry vehicle for space shuttle missions - Vol. 1, Part A
Costs and schedules for integral launch and reentry vehicle - Vol. 1, Part B
Technology identification for integral launch and reentry vehicles - Vol. 2
Integral launch and reentry vehicle integrated electronics system - Vol. 3, Part B
Characteristics of integral launch and reentry vehicles - executive summary
Summary of design of integral launch and reentry vehicle for space logistics - Vol. 1
Technology development requirements of integral launch and reentry vehicle for space logistics - Vol. 2
Environment and performance of integral launch and reentry vehicle for space logistics - Vol. 3
Design and subsystems analysis of integral launch and reentry vehicles for space logistics - Vol. 4
Technology and resources for development of integral launch and reentry vehicles for space logistics - Vol. 5
Leading edge design for hypersonic reentry vehicles