Would yield a pure.

Lower the Orbiter general- purpose computer is used to update inertial measurement unit integrated test article SLF microwave scanning beam landing system. 6-36 DEORBIT BURN 60 MIN TO TOUCHDOWN 70 km (43.5 MILES) 24 200 km/H (15 045 MPH) EXIT BLACKOUT 12 MIN TO.

Figure 6-5.—Mobile Launcher Platform and the J-2 engine, which was several centuries.