An Experimental Comparison of Three Typical MARS Entry Body Shapes on the Basis of Total Equilibrium Shock-Layer Radiation
1966
110 pages
Report
No indication
English
Physics , Spacecraft Trajectories & Flight Mechanics , Mars (planet) , Radiative heat transfer , Reentry body , Shock layer , Analysis , Angle , Apollo spacecraft , Attack , Ballistics , Blunt , Body , Cone , Distribution , Effect , Equilibrium , Heat , Layer , Mars , Measurement , Model , Pressure , Radiation , Radiative , Range , Reentry , Shape , Shock , Spacecraft , Trajectory , Transfer , Tube , Tunnel , Zero