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Nasda N-1
Nasda N-1 - Nasda N-1 - COSPAR 1975-082

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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: 7. Failures: 1. Success Rate: 85.71% pct. First Launch Date: 09 September 1975. Last Launch Date: 03 September 1982. LEO Payload: 1,200 kg. to: 185 km Orbit. Payload: 360 kg. to a: Geosynchronous transfer trajectory. Liftoff Thrust: 233,260 kgf. Total Mass: 131,330 kg. Core Diameter: 2.4 m. Total Length: 34.0 m. Flyaway Unit Cost $: 23.01 million. in 1985 unit dollars.


N Chronology


1975 Sep 9 - - 05:30 GMT. LV Configuration: N-1 s/n N-1(F). Launch Site: Tanegashima . Launch Complex: O.
1976 Feb 29 - - 03:30 GMT. LV Configuration: N-1 s/n N-2(F). Launch Site: Tanegashima . Launch Complex: O.
1977 Feb 23 - - 08:50 GMT. LV Configuration: N-1 s/n N-3(F). Launch Site: Tanegashima . Launch Complex: O.
1978 Feb 16 - - 04:00 GMT. LV Configuration: N-1 s/n N-4(F). Launch Site: Tanegashima . Launch Complex: O.
1979 Feb 6 - - 08:46 GMT. LV Configuration: N-1 s/n N-5(F). Launch Site: Tanegashima . Launch Complex: O. FAILURE: Third stage collided with ECS a.
1980 Feb 22 - - 08:35 GMT. LV Configuration: N-1 s/n N-6(F). Launch Site: Tanegashima . Launch Complex: O.
1982 Sep 3 - - 05:00 GMT. LV Configuration: N-1 s/n N-9(F). Launch Site: Tanegashima . Launch Complex: O.

Bibliography:



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Last update 12 March 2001.
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