Falcon 9 Launch Vehicle Payload User's Guide - SpaceX

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4.1.6. Geosynchronous Transfer Orbit (Kwajalein) Payload Mass (kg) 8000 7000 6000 5000 4000 3000 2000 1000 0 0 10000 20000 30000 40000 50000 60000 70000 80000 90000 100000 Apogee Altitude (km) with 185 km perigee (Kwajalein) Falcon 9 User’s Guide Figure 4‐6 ‐ Falcon 9 Block 2 Performance to Geosynchronous Transfer Orbit (Kwajalein) Table 4‐6 ‐ Falcon 9 Block 2 Performance to Geosynchronous Transfer Orbit (Kwajalein) Orbit Altitude Payload Mass (kg) Inclination (deg) (km) 9 5 0 10000 7203 6859 5750 20000 5638 5408 4618 30000 4935 4744 4074 35786 4682 4503 3875 40000 4537 4365 3759 50000 4282 4120 3552 60000 4103 3949 3407 70000 3972 3823 3299 80000 3871 3727 3216 90000 3792 3650 3150 100000 3727 3588 3097 9 deg inclination 5 deg inclination 0 deg inclination SCM 2008‐010 Rev. 1 Copyright – SpaceX 2009 24
4.1.7. Geosynchronous Transfer Orbit (Delta-Velocity To Go) [Cape] Payload Mass (kg) 5000 4500 4000 3500 3000 2500 2000 1500 1000 Falcon 9 User’s Guide 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 Delta‐V to GEO (meters/sec) from Cape Canaveral F9 without delta‐V mission kit (Cape) F9 with delta‐V mission kit (Cape) Figure 4‐7 ‐ Geosynchronous Transfer Orbit (Delta‐Velocity to Go) from Cape Table 4‐7 ‐ Geosynchronous Transfer Orbit (Delta‐Velocity to Go) from Cape 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) 1588 2972 1127 1400 1617 3325 1158 1600 1650 3660 1202 1900 1685 3963 1307 2600 1723 4216 1407 3200 1763 4405 1498 3600 1837 4536 1533 3700 1682 3900 SCM 2008‐010 Rev. 1 Copyright – SpaceX 2009 25
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: 4.1.5. 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
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

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