Reusable high-performance rocket engine combustion process.

LOOP LINES FUEL LINES Y Zr. Қ А % -— Y, 7% FUEL ISOLATION і 2 А VALVES (2) (APU SYSTEM 3) AND FILTERS FUEL SERVICING - ISOLATION RECEPTACLES VALVES (2) AND FILTER (1) | 7 / & SS асе APU SYSTEM 2 FUEL TANK = APU SYSTEM 1 1 Mission specialist 1 1/shift Payload specialist Oori 1to4 Crew tota! 3or4 4to7 AUS = inertial upper.