A launch phase random normal wind model is presented for delta wing, two-stage, space shuttle control system studies. Equations, data, and simulations for conventional launch studies are given as well as pitch and lateral equations and data for covariance analyses of the launch phase of MSFC vehicle B. Lateral equations and data for North American 130G and 134D are also included along with a high-altitude abort simulation.
Development of control systems for space shuttle vehicles. Volume 2: Appendixes
1971-09-01
Report
No indication
English
Design of H2-O2 space shuttle APU. Volume 2: Appendixes
NTRS | 1974
|Space industrialization. Volume 4: Appendixes
NTRS | 1978