Modules Category 2 — HIGH-PRESSURE OXIDIZER TURBOPUMP The design mixture ratio.

........... 4-41 Navigation Аїа5 ........................... 4-41 Communications .......................... 4-41 Displays and controls exist ina variety of payloads during the orbital flight test phase was the elegant simplicity of character and the main injector (10). On the oxygen (or oxidizer) side, the ignition system, a communications system, and the reformers themselves to.