The Sea Dragon was a 1962 design study for a very large reusable two-stage launch vehicle that would have lifted payloads to low Earth orbit from the open ocean. Robert Truax led the work while employed at Aerojet, as one of several designs in which a rocket is floated out to sea and launched from the water. The idea was a cheap heavy launcher, sometimes called a big dumb booster, built from inexpensive 8 mm steel sheet in an ordinary shipyard and towed to the launch site, where ballast tanks tipped it upright with the payload just above the waterline. At about 150 m long and 23 m wide it would have been the largest rocket ever built, with a first stage burning RP-1 and liquid oxygen and a second stage burning liquid hydrogen and oxygen. Its claimed payload was up to 550 tonnes to low Earth orbit. Despite interest at NASA and Todd Shipyards the design was never built.
Facts
PropulsionLiquid hydrogen and liquid oxygen 1 Engine Class StatusDesign only (never built) 1 Connections
Exemplifies
Source Sea Dragon (rocket) (Wikipedia)
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Source Encyclopedia Astronautica: Sea DragonEntry text, summaryQuote, Entry text, summary
American sea-launched heavy-lift orbital launch vehicle.
Sources
1. Encyclopedia Astronautica: Sea Dragon
Encyclopedia AstronauticaEntry text
designed by Robert Truax for Aerojet in 1962
Entry text, summary
American sea-launched heavy-lift orbital launch vehicle.
Entry text, outcome
Prospects for Sea Dragon essentially disappeared, and Aerojet could no longer fund it on IR&D.
Entry text, first stage
The launch vehicle would be fuelled with RP-1 kerosene in port
Entry text, second stage
burned LOX/LH2
Entry text, first stage, engine class
The first stage had a single pressure fed, thrust chamber of 36 million kgf thrust, burning LOX/Kerosene.
View the Source Sea Dragon (rocket) (Wikipedia)
In Group: Orbital Launch Vehicles, Lead, vehicle class
reusable two-stage sea-launched orbital super heavy-lift launch vehicle
Exemplifies: Orbital Spaceflight, Lead, mission
reusable two-stage sea-launched orbital super heavy-lift launch vehicle
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