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Aviation History
1962
1962 - 0091.PDF
FLIGHT International, 18 January 1962 91 6S 64, 28 29 30 31 32 33 34 35 36 37 3& 39 40 41 42 43 44 45 46 47 48 49 55 58 59 60 61 62 63 64 65 66 67 68 69 Rocketdyne LR-105 sustainer engine Fuel-circulation basket tubes form thrust chamber Steel hoop-stress bands (glass-fibre in later 105-5 engines) Sustainer-turboprop exhaust aspira tor shroud discharges fuel-rich gas into propulsive jet Lox delivery manifold (K-Monel) and check valve Fuel delivery manifold (K-Monel) Expansion and flexure bellows Sustainer Lox pump Sustainer fuel pump Flexible asbestos muff to protect interior during lift-off Turbine spinner, solid fuel (not on early engines) Turbopurnp gas generator Turbine started by (38) and run on fuel-rich Lox/fue! mix from (39) to drive (35) and (36) through gearbox Turbopump exhaust heat-exchanger heats GH from (6) Turbopump overboard drains Turbopump suspension Sustainer gimballing hydraulic actua tors Sustainer low-pressure oil tank feed ing h-p gear pump Booster jettison track (Quadrant 4) Booster jettison track (Quadrant 2) Jettison track A-frame Vernier engine, Rocketdyne LR-IOI, pivoting to govern roll (another in opposite quad at 180) Lox line to (49) Fuel line to (49) Vernier-engine fairing, protected against aerodynamic heating during climb Stub pod position in Quad 2 Main instrumentation pod in Quad 4 for electronics, radio and guidance Flush aerials for guidance and down- range telemetry Radio receivers Pressurized canisters for autopilot, guidance electronics, telemetry trans mitters, propel!ant-utilizatton com puter, range-safety system and tracking transponders Inter-pod cable ducts Locating anchors for (\ 12) Main umbilical connector (both sides of missile) Engine control and instrumentation cables Hydraulicand other lines to (49) Re-entry vehicle in-flight disconnect cable fairing Re-entry vehicle adapter, transition bay and upper umbilical socket Re-entry vehicle (General Electric Mk 3 shown) Retrorocket (both sides of missile) Fuel fill and drain coupling (Hadley- AiResearch) Fuel fill and drain adapter support Coupling muff and heat shield for (67) 70 Bracing struts for (67) 71 Lox fill and drain coupling (Hadley valve) 72 Lox fill and drain adapter support 73 Coupling muff and heat shield for (71) 74 Tie strut for (22) 75 Fuel supply bifurcation 76 Fuel pumps 77 Lox pumps 78 Lox feed line to and from tank 79 Turbopumps 80 Turbine spinner, solid fuel (not on early engines) 81 Gas generator serving both turbo- pumps 82 Turbopump oil-additive reservoir (not on early engines) 83 Turbopumps hung from booster air frame 84 Flexible exhaust bellows 85 Heat exchanger to heat GH from (6) 86 Exhaust stack discharges fuel-rich efflux outside reverse aerodynamic flow at base of missile 87 Turbopump overboard drains 88 Ties to react pipe thrust 89 Fuel to No I booster engine 90 Fuel to No 2 booster engine 91 Lox to No I booster engine 92 Lox to No 2 booster engine 93 Braided flexible hose 94 No I booster, Rocketdyne LR-89 95 No I booster combustion chamber 96 Thrust-chamber nozzles of basket- tube construction with steel bands (glass-fibre in LR-89-5) 97 Flexible asbestos muff to protect interior during lift-off 98 Lubricating-oil tank (one on each booster, feeding at about 601b sq in to h-p gear-pump) 99 Mam fuel check-valve 100 Gimbal mount and thrust pad 101 Gimbal pitch actuator 102 Gimbal yaw actuator 103 Integrated control package for hy draulic gimballing 104 Main thrust girders 105 Booster skin with external top-hat stringers 106 Plate frames 107 Cantilever beam for (102) 108 Retractable jettison-track roller units, running on (46) 109 Transverse tie-rods 110 Base bulkhead with insulating blanket 111 Vernier cable fairing 112 Explosive attachment bolts 113 Booster skirt fairing 114 Main launcher support and hold-down trunnions 115 Lower launcher hold-down anchorage 116 Doors to (114) slam shut after lift-off 117 Auxiliary support socket against wind-tilt 1(8 Ground rise-off disconnect panel (mainly purging systems) 119 Ground rise-off disconnect panel (mainly pressurization and instru mentation ' Sf£f
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