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Nasda N-2
Nasda N-2 - Nasda N-2 - COSPAR 1981-012

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Family: Delta. Country: Japan. Status: Hardware.

Licensed version of Delta built in Japan using both US and Japanese components.


Specifications

Launches: 8. Failures: 0. Success Rate: 100.00% pct. First Launch Date: 11 February 1981. Last Launch Date: 19 February 1987. LEO Payload: 2,000 kg. to: 185 km Orbit. Payload: 730 kg. to a: Geosynchronous transfer trajectory. Liftoff Thrust: 233,260 kgf. Total Mass: 132,690 kg. Core Diameter: 2.4 m. Total Length: 35.0 m. Flyaway Unit Cost $: 26.49 million. in 1985 unit dollars.


N-2 Chronology


1981 Feb 11 - - 08:30 GMT. LV Configuration: N-2 s/n N-7(F). Launch Site: Tanegashima . Launch Complex: O.
1981 Aug 10 - - 20:03 GMT. LV Configuration: N-2 s/n N-8(F). Launch Site: Tanegashima . Launch Complex: O.
1983 Feb 4 - - 08:37 GMT. LV Configuration: N-2 s/n N-10(F). Launch Site: Tanegashima . Launch Complex: O.
1983 Aug 5 - - 20:29 GMT. LV Configuration: N-2 s/n N-11(F). Launch Site: Tanegashima . Launch Complex: O.
1984 Jan 23 - - 07:58 GMT. LV Configuration: N-2 s/n N-12(F). Launch Site: Tanegashima . Launch Complex: O.
1984 Aug 2 - - 20:09 GMT. LV Configuration: N-2 s/n N-13(F). Launch Site: Tanegashima . Launch Complex: O.
1986 Feb 12 - - 07:55 GMT. LV Configuration: N-2 s/n N-14(F). Launch Site: Tanegashima . Launch Complex: O.
1987 Feb 19 - - 01:23 GMT. LV Configuration: N-2(2) s/n N-16(F). Launch Site: Tanegashima . Launch Complex: O.

Bibliography:



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Last update 12 March 2001.
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