This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com J-1


Family: H. Country: Japan. Status: Development.

All-solid rocket motor launch vehicle. Because of the high cost, an alternate J-1 F2 design was developed.


Specifications

LEO Payload: 850 kg. to: 250 km Orbit. at: 30.0 degrees. Liftoff Thrust: 158,000 kgf. Total Mass: 88,580 kg. Core Diameter: 1.8 m. Total Length: 33.1 m. Development Cost $: 100.00 million. in 1996 average dollars. Launch Price $: 45.00 million. in 1996 price dollars.



Bibliography:



Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .