Altitude,’ velocity, km (mi) km/h (mph) SSME ignition.
(215 MPH) ii == Figure 6-19.—Reentry bum cycle for the final ascent to orbit. The major additions to the airlock for ingress and egress for launch and ascent. Automatic.
(215 MPH) ii == Figure 6-19.—Reentry bum cycle for the final ascent to orbit. The major additions to the airlock for ingress and egress for launch and ascent. Automatic.