Max. Payload (kg)d |
Vehicle |
Stages: Engine/Motor |
Propellanta |
Thrust (kilonewtons)bc |
Max. Dia x Height (m) |
185-Km Orbit |
Geosynch. Transfer Orbit |
Sun- Synch. Orbite |
First Launchf |
Pegasus |
|
|
|
6.71x15.5h |
380 |
|
210 |
1990 |
|
|
|
|
|
280e |
|
|
|
|
1. Orion 50S 2. Orion 50 3. Orion 38 |
Solid Solid Solid |
484.9 118.2 31.9 |
1.28x2.66 1.28x2.66 0.97x1.34 |
|
|
|
|
Pegasus XL |
|
|
|
|
|
|
|
|
|
|
|
|
6.71x16.93 |
460 |
|
335 |
1994g |
|
1. Orion 50S-XL 2. Orion 50-XL 3. Orion 38 |
Solid Solid Solid |
743.3 201.5 31.9 |
1.28x10.29 1.28x3.58 0.97x1.34 |
350e |
|
|
|
Taurus |
|
|
|
|
|
|
|
|
|
|
|
|
2.34x28.3 |
1400 |
255 |
1020 |
Not scheduled |
|
0. Castor 120 1. Orion 50S 2. Orion 50 3. Orion 38 |
Solid Solid Solid Solid |
1687.7 580.5 138.6 31.9 |
2.34x11.86 1.28x8.88 1.28x2.66 0.97x1.34 |
1080e |
|
|
|
Delta II |
|
|
|
2.44x29.70 |
5089 |
1842i |
3175 |
1990, Delta-7925 [1960, Delta] |
(7920, 7925) |
|
|
|
|
3890e |
|
|
|
|
1. RS-270/A Hercules GEM (9) 2. AJ10-118K 3. Star 48Bj |
LOX/RP-1 N204/A-50 Solid |
1043.0 (SL) 487.6 (SL) 42.4 66.4 |
3.05x38.1 1.01x12.95 2.44x5.97 1.25x2.04 |
|
|
|
|
Atlas E |
|
|
|
3.05x28.1 |
820e |
|
910k |
1968, Atlas F [1958, Atlas LV-3A] |
|
|
|
|
|
1860e |
|
|
|
|
1. Atlas: MA-3 |
LOX/RP-1 |
1739.5 (SL) |
3.05x21.3 |
|
|
|
|
Atlas I |
|
|
|
4.2x43.9 |
|
2255 |
|
1990, I [1966, Atlas Centaur] |
|
1. Atlas: MA-5 2. Centaur I: RL10A-3-3A (2) |
LOX/RP-1 LOX/LH2 |
1952.0 (SL) 73.4/engine |
3.05x22.16 3.05x9.14 |
|
|
|
|
Atlas II |
|
|
|
4.2x47.5 |
6580 |
2810 |
4300 |
1991, II [1966, Atlas Centaur] |
|
|
|
|
|
|
5510e |
|
|
|
|
1. Atlas: MA-5A 2. Centaur II: RL10A-3-3A (2) |
LOX/RP-1 LOX/LH2 |
2110.0 (SL) 73.4/engine |
3.05x22.16 3.05x9.14 |
|
|
|
|
Atlas IIA |
|
|
|
4.2x47.5 |
6828 |
3062 |
4750 |
1992, Atlas IIA [1966, Atlas Centaur] |
|
|
|
|
|
|
6170e |
|
|
|
|
1. Atlas: MA-5A 2. Centaur II: RL10A-4 (2) |
LOX/RP-1 LOX/LH2 |
2110.0 (SL) 92.53/engine |
3.05x24.9 3.05x10.05 |
|
|
|
|
Atlas IIAS |
|
|
|
4.2x47.5 |
8640 |
3606 |
5800 |
1993, [1966, IIAS Atlas Centaur] |
|
|
|
|
|
7300e |
|
|
|
|
1. Atlas: MA-5A Castor IVA (4)j 2. Centaur II: RL10A-4 (2) |
LOX/RP-1 Solid LOX/LH2 |
2110.0 (SL) 433.6 (SL) 92.53/engine |
3.05x24.9 1.01X11.16 3.05x10.05 |
|
|
|
|