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Orbital Sciences Corporation
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UNITED STATES
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Vehicles
| Rank | Vehicle | Launches | Payload to LEO | First flight |
|---|---|---|---|---|
| 01 | Pegasus XL | 32 launches | 443 kg | 1994 |
| 02 | Minotaur I | 12 launches | 580 kg | 2000 |
| 03 | Pegasus XL HAPS | 5 launches | 443 kg | 1997 |
| 04 | Pegasus Hybrid | 4 launches | 350 kg | 1995 |
| 05 | Pegasus | 4 launches | 443 kg | 1990 |
| 06 | Minotaur-C 2110 | 2 launches | 1,380 kg | 2001 |
| 07 | Antares 110 | 2 launches | 4,450 kg | 2013 |
| 08 | Pegasus HAPS | 2 launches | 250 kg | 1991 |
| 09 | Antares 120 | 2 launches | 4,600 kg | 2014 |
| 10 | Minotaur-C 3110 | 1 launche | — | 2009 |
| 11 | Minotaur-C 1110 | 1 launche | 1,320 kg | 2000 |
| 12 | Minotaur-C 2210 | 1 launche | 1,380 kg | 1998 |
| 13 | Minotaur IV+ | 1 launche | 1,950 kg | 2011 |
| 14 | Minotaur-C 3210 | 1 launche | — | 2004 |
| 15 | Minotaur V | 1 launche | 1,735 kg | 2013 |
| 16 | Antares 130 | 1 launche | 5,100 kg | 2014 |
| 17 | Minotaur IV HAPS | 1 launche | 1,750 kg | 2010 |
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Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026