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Pegasus was an air-launched, small-lift launch vehicle developed by Orbital Sciences Corporation and later built and launched by Northrop Grumman. Pegasus was the world's first privately developed orbital launch vehicle. Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, Pegasus first flew in 1990 and last flew…
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Northrop Grumman Pegasus | Altitude | 200 km (120 mi) | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 75.3 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 68.6 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 75.6 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 69.4 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 68.5 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 131 + 110 seconds (2 burns) | 1.00 | infobox |
| Northrop Grumman Pegasus | Comparable | Electron, Vector-H, Falcon 1, LauncherOne | 1.00 | infobox |
| Northrop Grumman Pegasus | Cost per launch | US$40 million (2017) | 1.00 | infobox |
| Northrop Grumman Pegasus | Country of origin | United States | 1.00 | infobox |
| Northrop Grumman Pegasus | Derivative work | Minotaur-C | 1.00 | infobox |
| Northrop Grumman Pegasus | Diameter | 1.28 m (4 ft 2 in) Wing span: 6.7 m (22 ft) | 1.00 | infobox |
| Northrop Grumman Pegasus | Diameter | 0.97 m (3 ft 2 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Empty mass | 1,369 kg (3,018 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Empty mass | 416 kg (917 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Empty mass | 126 kg (278 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Failure | 3 | 1.00 | infobox |
| Northrop Grumman Pegasus | First flight | April 5, 1990 (Pegsat / NavySat) | 1.00 | infobox |
| Northrop Grumman Pegasus | Function | Small-lift launch vehicle | 1.00 | infobox |
| Northrop Grumman Pegasus | Gross mass | 16,383 kg (36,118 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Gross mass | 4,341 kg (9,570 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Gross mass | 872.3 kg (1,923 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | Standard: 16.9 m (55 ft 5 in) XL: 17.6 m (57 ft 9 in): 3 | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | 10.27 m (33 ft 8 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | 3.11 m (10 ft 2 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | 1.34 m (4 ft 5 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | 0.3 m (1 ft 0 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Last flight | July 3, 2026 (Swift rescue mission (LINK)) | 1.00 | infobox |
| Northrop Grumman Pegasus | Launch sites | Air launch to orbit from Cape Canaveral, Edwards, Gando, Kennedy, Kwajalein, Vandenberg or Wallops | 1.00 | infobox |
| Northrop Grumman Pegasus | Manufacturer | Orbital Sciences (1990–2015) | 1.00 | infobox |
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