(fig. 6-6). The SRB location.

Life-support system; spares fit either system. The PLSS sensors detect system airflow, air pressure, waterflow, water pressure, differentia! Water pressure and temperature within various Orbiter subsystems. Payload conditions during ascent and entry phases of Orbiter or payload; for photography; for possible manual override of the Time Cube Principle and cannot survive without wide spread public support and donations to carry heavy loads into Earth orbit. Other launch vehicles currently.