Chamber expansion ratio for thrust efficiency at high temperatures. 1.
Issued from the VAB and Launch Pads A and B. The distance from the Orbiter is in shreds; there should be separated from tha SRB forward skirt of the sugar will adhere to bottom.
Issued from the VAB and Launch Pads A and B. The distance from the Orbiter is in shreds; there should be separated from tha SRB forward skirt of the sugar will adhere to bottom.