Ohsumi
Spacecraft · Japan
Original archive entry. The text, images and links below are kept as they were written.

Credit: NASDA
Japanese technology satellite. Small engineering test satellites lofted by Japan's first indigenous launch vehicle. Technology satellite operated by ISAS, Japan. Launched 1966 - 1970.
More at: Ohsumi.
Related
- Family
- Technology, Technology satellite
- Country
- Japan
- Launch Sites
- Kagoshima, Kagoshima L
Chronology
4 events
1966 September 26
02:58 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. LV Family: Lambda. Launch Vehicle: Lambda 4S. FAILURE: Fourth stage attitude control failed.. Failed Stage: 4.- Ohsumi 1 - . Payload: L-4S-1. Mass: 26 kg (57 lb). Nation: Japan. Agency: ISAS. Class: Technology. Type: Navigation technology satellite. Spacecraft: Ohsumi. Decay Date: 1966-09-26 . Apogee: 400 km (240 mi).
1966 December 20
02:20 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. LV Family: Lambda. Launch Vehicle: Lambda 4S. FAILURE: Fourth stage failed to ignite.. Failed Stage: 4.- Ohsumi 2 - . Payload: L-4S-2. Mass: 26 kg (57 lb). Nation: Japan. Agency: ISAS. Class: Technology. Type: Navigation technology satellite. Spacecraft: Ohsumi. Decay Date: 1966-12-19 . Apogee: 400 km (240 mi).
1967 April 13
Launch Site: Kagoshima. Launch Complex: Kagoshima L. LV Family: Lambda. Launch Vehicle: Lambda 4S. FAILURE: Fourth stage failed to ignite.. Failed Stage: 4.- Ohsumi 3 - . Payload: L-4S-3. Mass: 26 kg (57 lb). Nation: Japan. Agency: ISAS. Class: Technology. Type: Navigation technology satellite. Spacecraft: Ohsumi. Decay Date: 1967-04-13 . Apogee: 200 km (120 mi).
1969 September 22
02:10 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. LV Family: Lambda. Launch Vehicle: Lambda 4S. FAILURE: Fourth stage control system malfunction after third stage collided with fourth stage.. Failed Stage: 4.- Ohsumi 4 - . Payload: L-4S-4. Mass: 25 kg (55 lb). Nation: Japan. Agency: ISAS. Class: Technology. Type: Navigation technology satellite. Spacecraft: Ohsumi. Decay Date: 1969-09-22 . Apogee: 400 km (240 mi).