Falcon 9 Launch Vehicle Payload User's Guide - SpaceX

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Table 2‐1 ‐ Falcon 9 Launch Vehicle (Block 2) Dimensions and Characteristics Falcon 9 User’s Guide Characteristic Structure Stage 1 Stage 2 Length 180 feet [55m] (both stages with fairing & interstage) Diameter 12 feet [3.66m] Type LOX tank ‐ monococque; Fuel tank ‐ stringer and ring frame Monococque Material Propulsion Aluminum lithium Aluminum lithium Engine Type Liquid, gas generator Liquid, gas generator Engine Manufacturer SpaceX SpaceX Engine Designation Merlin 1C Merlin Vacuum Number of engines 9 1 Propellant Liquid oxygen/Kerosene (RP‐1) Liquid oxygen/Kerosene (RP‐1) Thrust 1,125,000 lbf (sea level) [5MN] 100,000 lbf (vacuum) [445kN] Propellant feed system Turbopump Turbopump Throttle capability No Yes (60‐100%) Restart capability No Yes ‐ 2 restarts Tank pressurization Thrust Vector Control Heated helium Heated helium Pitch, Yaw Gimbaled engines Gimbaled engine Roll Reaction Control System Gimbaled engines Turbine exhaust duct (gimbal) Propellant Not applicable Monomethyl hydrazine, nitrogen tetroxide Thrusters Not applicable Draco (4) Thrust Staging Not applicable 90 lbf [400N] each Nominal burn time 170 sec 354 sec Shutdown process Commanded shutdown Commanded shutdown Stage separation system Pneumatically actuated mechanical collets Not applicable SCM 2008‐010 Rev. 1 Copyright ‐‐ SpaceX 2009 10
2.2. Vehicle Axes/Attitude Definitions C Band 90 deg S ‐Band 60 deg UHF 120 deg True North (10 deg app .) Positive Clocking Angle TAA ‐3C (Telemetry ) +Z (0 deg) FPS 16 (Radar ) FTS Transmitter JD Missile Tracking Annex Figure 2‐1 ‐ Falcon 9 launch vehicle layout and coordinate system SCM 2008‐010 Rev. 1 Copyright ‐‐ SpaceX. 2009 Q I Transporter / Errector 9 8 7 6 Q IV 5 4 Q II Q III 3 2 1 Notes ‐ Vehicle as seen from above ‐ Vehicle coordinate frame as shown , with the X axis being the vehicle longitudinal axis , positive forward . This coordinate frame is aligned with the Erector 30 . 8° UHF 300 deg C ‐Band 270 deg +Y S ‐Band 240 deg Fairing Split Line 292 .5 deg Falcon 9 User’s Guide 11
Page 1 and 2: Falcon 9 Launch Vehicle Payload Use
Page 3 and 4: Falcon 9 User’s Guide 5. General
Page 5 and 6: Falcon 9 User’s Guide Our design
Page 7 and 8: Falcon 9 User’s Guide rocket‐ g
Page 9: Falcon 9 User’s Guide crewed laun
Page 13 and 14: Figure 3‐3 ‐ Space Launch Compl
Page 15 and 16: Falcon 9 User’s Guide 3.3. Space
Page 17 and 18: Falcon 9 User’s Guide 3.5. Test F
Page 19 and 20: 4.1.1. Low Earth Orbit Payload Mass
Page 21 and 22: 4.1.3. Sun Synchronous Payload Mass
Page 23 and 24: 4.1.5. Geosynchronous Transfer Orbi
Page 25 and 26: 4.1.7. Geosynchronous Transfer Orbi
Page 27 and 28: Falcon 9 User’s Guide 4.2. Sample
Page 29 and 30: Falcon 9 User’s Guide 4.3. Mass P
Page 31 and 32: 5.1.3. Payload Separation Falcon 9
Page 33 and 34: AXIAL (G) -2, 3.5 -2, -1.5 -0.5, 6
Page 35 and 36: Figure 5‐4 ‐ Falcon 9 acoustic
Page 37 and 38: Function Table 5‐2 ‐ Falcon 9 L
Page 39 and 40: Freq (MHz) E Field Limit (dBμV/m)
Page 41 and 42: Falcon 9 User’s Guide propellant
Page 43 and 44: 5.3.2. Test Fittings and Fitcheck P
Page 45 and 46: Figure 5‐9 ‐ Spacecraft to Laun
Page 47 and 48: Falcon 9 User’s Guide encapsulati
Page 49 and 50: Launch Vehicle Ops Ground Ops Paylo
Page 51 and 52: Falcon 9 User’s Guide • Process
Page 53 and 54: Falcon 9 User’s Guide replaced wi
Page 55 and 56: 6.2. Spacecraft Transport to Launch
Page 57 and 58: Choice of 2 more consoles in these
Page 59 and 60: 6.3.1. Mission Integration Plan Tab
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7. Safety 7.1. Safety Requirements
Page 63 and 64:
Payload Information Payload Name/Ti
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Do you have a Spacecraft Separation
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6. Please describe the RF systems t
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Falcon 9 User’s Guide 9.2. List o
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