Dynamics and Thermodynamics of Planetary Entry |
Contents
DYNAMICS AND THERMODYNAMICS OF PLANETARY | 1 |
PART I | 14 |
THE UNIFIED SOLUTION OF ENTRY DYNAMICS | 27 |
Copyright | |
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Common terms and phrases
ablation aerodynamic heating altitude density Analytical approximate solution angles of inclination ballistic entry boundary layer Chapman Chapter coefficient convective dHav dt dHs dt drag drag coefficient dt max dv dt Earth Earth's atmosphere ENTRY AT CONSTANT entry at large entry at small entry solutions exact numerical machine flight path gliding entry gRo V2 heat transfer heating rate initial angles initial entry input per unit large angles latent heat lift lift coefficient lift force lift-drag ratio maximum deceleration occurs minor circle missile Numerical exact solution numerical machine calculations obtains overshoot boundary parameter perigee planet planetary atmosphere planetary entry problem radiation satellite second order solution shield shown in Figure small angles stagnation point sublimation Substituting Equation surface total heat trajectory undershoot unit area V₁ V2 gRo values vehicle Velocity ratio VgRo тв