Falcon 9 Launch Vehicle Payload User's Guide - SpaceX

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4.1.8. Geosynchronous Transfer Orbit (Delta-Velocity To Go) [Kwajalein] Payload Mass (kg) 5000 4500 4000 3500 3000 2500 2000 1500 1000 500 0 Falcon 9 User’s Guide 1100 1150 1200 1250 1300 1350 1400 1450 1500 1550 Delta‐V to GEO (meters/sec) from Kwajalein F9 without delta‐V mission kit (Kwaj) F9 with delta‐V mission kit (Kwaj) Figure 4‐8 ‐ Geosynchronous Transfer Orbit (Delta‐Velocity to Go) from Kwaj Table 4‐8 ‐ Geosynchronous Transfer Orbit (Delta‐Velocity to Go) from Kwaj Without delta-V mission kit With delta-V mission kit Delta-V to GSO (m/s) Payload Mass (kg) Delta-V to GSO (m/s) Payload Mass (kg) 1479 3875 1196 3300 1491 4503 1325 4000 1519 4682 1395 4100 1444 4200 SCM 2008‐010 Rev. 1 Copyright – SpaceX 2009 26
Falcon 9 User’s Guide 4.2. Sample Mission Profiles Each mission is unique in its flight profile. However, a typical flight profile for a maximum‐capability geosynchronous transfer orbit mission (including a delta‐V mission kit) is shown in the Figure 4‐9, below, and in Table 4‐9. Stage Separation T+176.2 sec 2 engine shutdown T+155.5 sec Liftoff (Cape Canaveral) T=0.0 sec Main Engine CutOff T+174.2 sec Fairing Separation T+199.2 sec 2 nd Stage Engine Start #1 T+179.2 sec Coast T+476-1488sec 2 nd Stage Engine CutOff #1 T+475.9 sec 2 nd Stage Engine Start #2 T+1488.6 sec 2 nd Stage Engine CutOff #2 T+1544.6 sec Figure 4‐9 ‐ Falcon 9 Sample Flight Profile, Geosynchronous Transfer Orbit Mission RCS Burn T+19913.2 – 20968.8 sec Payload Sep T+20978.8 sec SCM 2008‐010 Rev. 1 Copyright ‐‐ SpaceX 2009 27
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 and 10: Falcon 9 User’s Guide crewed laun
Page 11 and 12: 2.2. Vehicle Axes/Attitude Definiti
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: 4.1.7. Geosynchronous Transfer Orbi
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
Page 61 and 62: 7. Safety 7.1. Safety Requirements
Page 63 and 64: Payload Information Payload Name/Ti
Page 65 and 66: Do you have a Spacecraft Separation
Page 67 and 68: 6. Please describe the RF systems t
Page 69 and 70: Falcon 9 User’s Guide 9.2. List o

Falcon 9 Launch Vehicle Payload User's Guide - SpaceX

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