R-3896-1 A SUPPLEMENT TECHNICAL MANUAL ENGINE DATA F·1 ROCKET ENGINE (TITLE UNCLASSIFIED) (ROCKETDYNE) (HEROICRELICS.ORG) ;~:m/GRADE D TO It UNClASSIRED ~ w DO 254 DA TE D 11 PER CONTRAa No N~S B- ~8 - 6', AND HAS - B_ 5604· - - 8734 THIS PUBLICATION SUPPLEMENTS TECHNICAL MANUAL R·3896·1 DATED 31 MARCH 1967. PUBLISHED UNDER AUTHORITY OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NOTICE: This material contains information affecting the National Defense of the United States within the meaning of the Espionage Laws, Title 18, U.S.c., Sections 793 and 794, the transmission or revelation of which in any manner to an unauthorized person is prohibited by law. This page IS Unclassified 13 FEBRUARY 1968 DOWNGRADED AT 3 YEAR INTERVALS; DECLASSIFIED AFTER 12 YEARS. D.O.D. DIR. 5200.10. LIST OF EFFECTIVE PAGES TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 6 CONSISTING OF THE FOLLOWING: Page Page Page Issue No. Issue No. No. Issue Ti tle .... ..... ... ... .. Original A . • . .•. .. • .• . • .. •• . .•. Original 1-1 thru 1- 4 .............. Or iginal A Section I GAS GENERATOR ~ INJECTOR FUEL INLET HOUSING TEE INTERFACE GAS GENERATOR BALL VALVE INTERFACE FUEL MANIFOLD- FUEL RING SEAL MONITOR PORT FUEL DISK FUEL RING SECTION A-A ~-'--U OXIDIZER RING FUEL RING OXIDIZER RING ' F~L~G ~B~B~F~L~G SEcrlON - RING DOUBLET ORIFICE IMPINGEMENT PATTERN ~ ENGINES NOT INC ORPORATING MD140 CHANGE (TYPICAL) Fl-l-l Figure 1-14. (C) Gas Generator Injector--Cutaway View 1-1 Section I HYPERGOL AND ~GIC IGNITER FUEL INLET (IGN) E,D FUEL FE PASSAGE (TYPICAL) SECTION A-A CGle ~ TYPICAL RIGHT- ~HAND DIVIDERS ~ ~TYPICALLEFr_~ ~HAND DIVIDERS ~TYPICAL LEFT- DETAIL ~HANDDIVIDERS~~ B DETAIL r;"'lTYPICAL RIGHT- ~ HAND DIVIDERS ~/ - E ~ DETAIL P2'1TYPICAL C~NTER C DETAIL ~ DIVIDERS ~ F o DETAIL D (!] ENGINES NOT INCORPORATING MD22 CHANGE ~ ENGINES INCORPORATING MD~ CHANGE o ENGINES NOT INCORPORATING MD147 CHANGE 209241 -C- 2A Figure 1-24. (C) Thrust Chamber Injector--Cutaway View (Sheet 1 of 2) 1-2 Section I COMPARTMENT IDENTIFlC ATION NUMBER (TYPICAL) THRUST CHAMBER THROAT PLUG ATTACH HOLE -53 - 31 -29 -27 -25 - 23 -21 - 19 X INDEX PIN -33 LEGEND r"i','iii"",',',',,1 FUEL mNGS [==:J OXIDIZER mNGS 209241-C-lD Figure 1-24. (C) Thrust Chamber Injector--Cutaway View (Sheet 2 of 2) 1-3 Section I FIRST-STAGE NOZZLE FUEL TORQUE BEARING INLET SUPPORT PRIMARY FUEL GEAR SEAL DRAIN_ ASSEMBLY (2 PLACES LOCATED 180 DEGREES APART) THRUST WASHER, SPACER LOCK & NUT SHAFT BEARING SLINGER RETAINER AND HEATER ASSEMBLY BAFFLE RING SECOND -STAGE WHEEL FIRST -STAGE WHEEL PISTON RINGS OXIDIZER IMPELLER OXIDIZER VOLUTE HOT-GAS DIAPHRAGM NO. 3 BEARING LUBE DRAIN HOT GAS MANIFOLD NO. 3 BEARING PRIMARY OXIDIZER SEAL DRAIN -PRIMARY FUEL SEAL NO. 1 AND NO. 2 LUBE DRAIN OXIDIZER INTERMEDIATE PURGE (LOCATED 2 PLACES SEAL 180 DEGREES APART) SLINGER AND GASKET NUT, RING, LOCK AND GASKET 458800-C -1 B Figure 1-30. (C) Turbopump--Cutaway View 1-4 .