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The Sea Dragon was a 1962 conceptualized design study for a reusable two-stage sea-launched orbital super heavy-lift launch vehicle. The project was led by Robert Truax while working at Aerojet, one of several designs he created intended to be launched by floating the rocket in the ocean. Although there was some interest at both NASA and Todd Shipyards…
Design, Sea Dragon in fiction & Overview
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Sea Dragon (rocket) | Altitude | 229 km (124 nmi) | 1.00 | infobox |
| Sea Dragon (rocket) | Burn time | 81 seconds | 1.00 | infobox |
| Sea Dragon (rocket) | Burn time | 260 seconds | 1.00 | infobox |
| Sea Dragon (rocket) | Burn time | 1340 seconds | 1.00 | infobox |
| Sea Dragon (rocket) | Country of origin | United States | 1.00 | infobox |
| Sea Dragon (rocket) | Diameter | 23 m (75 ft) | 1.00 | infobox |
| Sea Dragon (rocket) | Function | Orbital super heavy-lift launch vehicle | 1.00 | infobox |
| Sea Dragon (rocket) | Height | 150 m (490 ft) | 1.00 | infobox |
| Sea Dragon (rocket) | Mass | 18,143 t (39,998,000 lb) | 1.00 | infobox |
| Sea Dragon (rocket) | Mass | 550 t (1,210,000 lb) | 1.00 | infobox |
| Sea Dragon (rocket) | Maximum thrust | 355.8 MN (80,000,000 lbf) at sea level | 1.00 | infobox |
| Sea Dragon (rocket) | Maximum thrust | 62.80 MN (14,120,000 lbf) vacuum | 1.00 | infobox |
| Sea Dragon (rocket) | Maximum thrust | 236.6 kN (53,200 lbf) each | 1.00 | infobox |
| Sea Dragon (rocket) | Powered by | 1 engine | 1.00 | infobox |
| Sea Dragon (rocket) | Powered by | 4 engines | 1.00 | infobox |
| Sea Dragon (rocket) | Propellant | RP-1 / LOX | 1.00 | infobox |
| Sea Dragon (rocket) | Propellant | LH2 / LOX | 1.00 | infobox |
| Sea Dragon (rocket) | Specific impulse | 242 s | 1.00 | infobox |
| Sea Dragon (rocket) | Specific impulse | 409 s | 1.00 | infobox |
| Sea Dragon (rocket) | Stages | 2 | 1.00 | infobox |
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