A minimum heating flight mode for high lateral range space shuttle entries including the effects of transition
Minimum heating flight mode for high lateral range space shuttle reentry based on boundary layer transition criteria
Moote, J. D.↗
Engineering topics
Moote, J. D.
Publications and source records attributed to Moote, J. D..
Apollo entry aerodynamics.
Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Crowder, R. S.↗
Apollo entry aerodynamics.
Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Crowder, R. S.↗