K150
Sounding rocket. Year: 1958. Country: Japan.

1/1.6 subscale test rocket used in development of the Kappa 9L sounding rockets.

Launches: 7. Success Rate: 100.00%. First Launch Date: 1958-04-08. Last Launch Date: 1962-08-01. Apogee: 5.00 km (3.10 mi). Total Mass: 100 kg (220 lb). Core Diameter: 0.15 m (0.49 ft). Total Length: 4.00 m (13.10 ft).

K150 Chronology

1958 April 8 - 01:31 GMT - Launch Site: Akita. Launch Vehicle: K150. LV Configuration: K150 K150S-1.

  • Test mission Nation: Japan. Agency: ISAS. Apogee: 6.00 km (3.70 mi). References: 1140.
1958 April 24 - 00:30 GMT - Launch Site: Akita. Launch Vehicle: K150. LV Configuration: K150 K150T-1.
  • Test mission Nation: Japan. Agency: ISAS. Apogee: 6.00 km (3.70 mi). References: 1140.
1958 April 24 - 04:00 GMT - Launch Site: Akita. Launch Vehicle: K150. LV Configuration: K150 K150T-2.
  • Test mission Nation: Japan. Agency: ISAS. Apogee: 6.00 km (3.70 mi). References: 1140.
1958 May 27 - 03:45 GMT - Launch Site: Akita. Launch Vehicle: K150. LV Configuration: K150 K150G.
  • Test mission Nation: Japan. Agency: ISAS. Apogee: 5.00 km (3.10 mi). References: 1140.
1960 Dec - Launch Site: Akita. Launch Vehicle: K150. LV Configuration: K150 SP-150-1.
  • K-9L 1/1.6 Model test flight Nation: Japan. Agency: ISAS. Apogee: 5.00 km (3.10 mi). References: 1145.
1960 Dec - Launch Site: Akita. Launch Vehicle: K150. LV Configuration: K150 SP-150-2.
  • K-9L 1/1.6 Model test flight Nation: Japan. Agency: ISAS. Apogee: 5.00 km (3.10 mi). References: 1145.
1962 Aug - Launch Site: Kagoshima. Launch Vehicle: K150. LV Configuration: K150 AT-150.
  • Test mission Nation: Japan. Agency: ISAS. Apogee: 5.00 km (3.10 mi). References: 1142.
 
 
 
 
 
 
 
 
 
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