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Jarvis Booster
Jarvis Booster - Jarvis Launch Vehicle

Credit: Hughes. 7,333 bytes. 68 x 387 pixels.



Family: Saturn V. Country: USA. Status: Study 1985.

Launch vehicle planned for Pacific launch based on Saturn V engines, tooling. Masses, payload estimated.


Specifications

LEO Payload: 38,000 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 13,000 kg. to a: Geosynchronous transfer trajectory. Liftoff Thrust: 1,376,130 kgf. Total Mass: 1,154,000 kg. Core Diameter: 8.4 m. Total Length: 58.0 m. Flyaway Unit Cost $: 260.00 million. in 1985 unit dollars.



Bibliography:



Jarvis launch padJarvis launch pad - Jarvis launc pad on Christmas Island in the mid-Pacific

Credit: Hughes. 10,110 bytes. 218 x 179 pixels.



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Last update 12 March 2001.
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