Spreadsheet: 09253d18-87c9-4a5a-8b17-c0bda9279e85
Sheet: LV Accuracies

Launch Vehicle Insertion Accuracies
 |  |  |  |  |  |  |  | Orbit Parameters | Rb (m) | Ra (m) | DelV a | DelV b | V at b
DNEPR |  |  |  |  |  |  |  | Case 1
Assumptions: circular obrit without a yaw maneuver, with 0.933 probabiliy |  |  |  |  |  |  |  | Case 2
 | Orbital Parameters |  | Typical Circular Orbits |  |  |  |  | Case 3
 |  | H = 300 km, inc = 98 degrees | H = 600 km, inc = 98 degrees | H = 900 km, inc = 65 degrees |  |  |  | Case 4
 | Altitude, km | ± 4.0 | ± 5.5 | ± 10.0
 | Period of revolution, sec. | ± 3.0 | ± 4.0 | ± 6.5
 | Inclination, deg. | ± 0.040 | ± 0.045 | ± .050
 | RAAND, deg | ± 0.050 | ± 0.060 | ± 0.070 |  |  |  | Orbital Parameters | H = 1000 km, inc = 0 deg.
 |  |  |  |  |  |  | Case 1 | Altitude, m ± | 100000
Delta IV Family |  |  |  |  |  |  |  | Period of revolution, sec. ± | 7.5
 | Orbit | Parameter | 3-σ Accuracy |  |  |  |  | Inclination, deg. ± | 0.052
 | GTO | Perigee altitude | ±5.6 km |  |  |  |  | RAAN, deg. ± | 0.06
 | 185 km x 35,786 km at 27 deg, ascending node inj | Apogee altitude | ± 93 km |  |  |  |  |  | H = 1000 km, inc = 28-62 deg.
 |  | Inclination | ± 0.03 deg |  |  |  | Case 2 | Altitude, m ± | 80000
 | LEO | Perigee altitude | ± 7.4 km |  |  |  |  | Period of revolution, sec. ± | 7.5
 | 500 km circular at 90 deg | Apogee altitude | ± 7.4 km |  |  |  |  | Inclination, deg. ± | 0.052
 | GEO | Inclination | ± 0.04 deg |  |  |  |  | RAAN, deg. ± | 0.074
 | 35,786 km circular at 4 deg | Altitude | ± 130 km |  |  |  |  |  | H = 35786 km, inc = 0 deg.
 |  | Inclination | ± 0.07 deg |  |  |  | Case 3 | Altitude, m ± | 180000
 |  | Eccentricity | ± 0.005 |  |  |  |  | Period of revolution, sec. ± | 7.5
 |  |  |  |  |  |  |  | Inclination, deg. ± | 0.07
EUROCKOT |  |  |  |  |  |  |  | RAAN, deg. ± | 0.06
Orbit 1: 300 km orbital altitude single-impulse injection scheme (direct injection) | Error Type | Orbit 1 | Orbit 2 |  |  |  |  |  | H = 35786 km, inc = 28-62 deg.
Orbit 2: 700 km orbital altitude two-impulse injection scheme (injection with coast phase) | Orbita altitude | ± 3.0 km | ± 6 km |  |  |  | Case 4 | Altitude, m ± | 200000
 | Inclination | ± 0.03 deg | ± 0.05 |  |  |  |  | Period of revolution, sec. ± | 7.5
 |  |  |  |  |  |  |  | Inclination, deg. ± | 0.075
Pegasus XL | Configuration | Insertion Apse Altitude | Non-insertion Apse Altitude | Semi-major Axis | Inclination |  |  | RAAN, deg. ± | 0.074
 | Pegasus XL | ± 10 km | ± 80 km | ± 45 km | ± 0.15 deg
 | Pegasus XL with HAPS | ± 15 km | ± 15 km | ± 15 km | ± 0.08 deg
Minotaur | Error Type | Tolerance (Worst Case)
 | Altitude (Insertion Apse) | ± 18.5 km
 | Altitude (Non-insertion Apse) | ± 92.6 km
 | Altitude (Mean) | ± 55.6 km
 | Inclination | ± 0.2 deg
 | Error Type |  | Angle | Rate
 | 3-axis | [NAME] | ± 1.0 deg | ± 0.5 deg/sec
 |  | Pitch | ± 1.0 deg | ± 0.5 deg/sec
 |  | Roll | ± 1.0 deg | ± 0.5 deg/sec
 | Spinning | Spin Axis | ± 1.0 deg | < 10 rpm
 |  | Spin Rate |  | 3 deg/sec
Taurus II | Error Type |  | Angle | Rate
 | 3-Axis | [NAME] | [NAME] | ± 0.5 deg/sec
 |  | Pitch | [NAME] | ± 0.5 deg/sec
 |  | Roll | [NAME] | ± 0.5 deg/sec
 | Spinning | Spin Axis | [NAME] | < 10 rpm
 |  | Spin Rate |  | ± 3 deg/sec
Start-1 | Orbital Parameter | Orbital Parameter Deviation
 |  | Standard LV configuration | LV configuration without PBPS
 | Orbital altitude, km
 | at injection point | ± 5 | ± 5
 | opposite of injection point | ± 5 | ± 85
 | Orbit inclination, arc. Min | ± 3 | ± 3
Delta II | Error Type | Error
Assumptions: two-stage mission to low-earth orbit | Perigee altitude, km | ± 25.0
 | Apogee altitude, km | ± 9.5
 | Orbit inclination , deg | ± 0.05
 | [NAME] (m/s) | Plane Change Delta -V (m/s) | Delta-V to transfer from fairing to correct orbit, worst-case altitude change and plane change (m/s) | Margin (25%) | Delta-V (m/s)
Case 1 |  |  |  | 0.25
Case 2 |  |  |  | 0.25
Case 3 |  |  |  | 0.25
Case 4 |  |  |  | 0.25
Propellant Required to Position in Correct Orbit | Final Mass After Burn (kg) |  | Mass of Propellant For Correction Out of LV Fairing (kg) | Margin (%) | Mass of Propellant For Correction Out of LV Fairing After Margin (kg)
Case 1 |  | Air |  | 0.15
 |  | Argon (Ar) |  | 0.15
 |  | C02 |  | 0.15
 |  | He |  | 0.15
 |  | H2 |  | 0.15
 |  | N2 |  | 0.15
 |  | O2 |  | 0.15
 |  | Butane |  | 0.15
 |  | Propane |  | 0.15
 |  | 2.3 kW |  | 0.15
 |  | 0.06 kW |  | 0.15
 |  | GREEN LMP-101X |  | 0.15
 |  | GREEN LMP-102 |  | 0.15
 |  | GREEN LMP-103X |  | 0.15
 |  | GREEN ADN/Methanol, 26% water |  | 0.15
 |  | GREEN HAN/Mehtanol, 26% water |  | 0.15
 |  | GREEN HAN/Glycine, 26% water |  | 0.15
 |  | [NAME], 60% Amm. Diss. |  | 0.15
Case 2 |  | Air |  | 0.15
 |  | Argon (Ar) |  | 0.15
 |  | C02 |  | 0.15
 |  | He |  | 0.15
 |  | H2 |  | 0.15
 |  | N2 |  | 0.15
 |  | O2 |  | 0.15
 |  | Butane |  | 0.15
 |  | Propane |  | 0.15
 |  | 2.3 kW |  | 0.15
 |  | 0.06 kW |  | 0.15
 |  | GREEN LMP-101X |  | 0.15
 |  | GREEN LMP-102 |  | 0.15
 |  | GREEN LMP-103X |  | 0.15
 |  | GREEN ADN/Methanol, 26% water |  | 0.15
 |  | GREEN HAN/Mehtanol, 26% water |  | 0.15
 |  | GREEN HAN/Glycine, 26% water |  | 0.15
 |  | [NAME], 60% Amm. Diss. |  | 0.15
Case 3 |  | Air |  | 0.15
 |  | Argon (Ar) |  | 0.15
 |  | C02 |  | 0.15
 |  | He |  | 0.15
 |  | H2 |  | 0.15
 |  | N2 |  | 0.15
 |  | O2 |  | 0.15
 |  | Butane |  | 0.15
 |  | Propane |  | 0.15
 |  | 2.3 kW |  | 0.15
 |  | 0.06 kW |  | 0.15
 |  | GREEN LMP-101X |  | 0.15
 |  | GREEN LMP-102 |  | 0.15
 |  | GREEN LMP-103X |  | 0.15
 |  | GREEN ADN/Methanol, 26% water |  | 0.15
 |  | GREEN HAN/Mehtanol, 26% water |  | 0.15
 |  | GREEN HAN/Glycine, 26% water |  | 0.15
 |  | [NAME], 60% Amm. Diss. |  | 0.15
Case 4 |  | Air |  | 0.15
 |  | Argon (Ar) |  | 0.15
 |  | C02 |  | 0.15
 |  | He |  | 0.15
 |  | H2 |  | 0.15
 |  | N2 |  | 0.15
 |  | O2 |  | 0.15
 |  | Butane |  | 0.15
 |  | Propane |  | 0.15
 |  | 2.3 kW |  | 0.15
 |  | 0.06 kW |  | 0.15
 |  | GREEN LMP-101X |  | 0.15
 |  | GREEN LMP-102 |  | 0.15
 |  | GREEN LMP-103X |  | 0.15
 |  | GREEN ADN/Methanol, 26% water |  | 0.15
 |  | GREEN HAN/Mehtanol, 26% water |  | 0.15
 |  | GREEN HAN/Glycine, 26% water |  | 0.15
 |  | [NAME], 60% Amm. Diss. |  | 0.15