Re-entry and Planetary Entry Physics and Technology, Volume 1Springer-Verlag New York, 1968 - Space vehicles |
Contents
reentry and planetary entry has resulted in many significant advances | 1 |
Dynamics Thermodynamics Physics and Radiation Part 2 Entry Abla | 15 |
Part One Entry Dynamics Thermodynamics | 17 |
Copyright | |
3 other sections not shown
Other editions - View all
Common terms and phrases
ablation aerodynamic heating altitude altitude density analytical approximate solution angle of elevation angles of inclination Astrodynamic axis ballistic entry boundary layer Chapman circular orbit velocity Co-Planar coefficient convective cos² drag drag coefficient Earth electrons energy Entry at Constant equations equilibrium flight flow ft/sec gasdynamic Gedeon gliding entry heat conduction heat input heat transfer heating rate hypersonic initial angles initial entry integration k₁ Kepler Number large angles launch radius lift lift-drag ratio magnetic field mass loss maximum deceleration Norair Report Numerical exact solution obtains optically thick optimum Order Theory parameter perigee planet planetary atmosphere plasma problem Re-Entry Reference region satellite second order solution Section shield shock wave shown in Figure sin² species speed stagnation point Substituting Eq surface temperature thermal radiation tion trajectory transverse waves true anomaly V₁ variables vehicle