Japanese all-solid orbital launch vehicle. Five stage vehicle consisting of 2 x SB-310 + 1 x L735 + 1 x L735(1/3) + 1 x L500 + 1 x L480S
Status: Retired 1970. First Launch: 1966年09月26日. Last Launch: 1970年02月11日. Number: 5 . Payload: 26 kg (57 lb). Thrust: 970.00 kN (218,060 lbf). Gross mass: 9,400 kg (20,700 lb). Height: 16.50 m (54.10 ft). Diameter: 0.74 m (2.42 ft). Apogee: 5,000 km (3,100 mi).
LEO Payload: 26 kg (57 lb).
Family:
all-solid,
orbital launch vehicle.
Country:
Japan.
Spacecraft:
Ohsumi,
Osumi.
Launch Sites:
Kagoshima,
Kagoshima L.
Stages:
L500,
L735,
L735(1/3),
SB-310,
L480S.
Agency:
ISAS.
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年09月26日 . 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年12月19日 . 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年04月13日 . 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年09月22日 . Apogee: 400 km (240 mi).
1970 February 11 - .
04:25 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima L.
LV Family:
Lambda.
Launch Vehicle:
Lambda 4S.
- Ohsumi 5 - .
Payload: L-4S-5. Mass: 12 kg (26 lb). Nation: Japan.
Agency: ISAS.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: Osumi.
Decay Date: 2003年08月02日 . USAF Sat Cat: 4330 . COSPAR: 1970-011A. Apogee: 2,440 km (1,510 mi). Perigee: 323 km (200 mi). Inclination: 31.00 deg. Period: 113.40 min. Engineering tests. Engineering test for the launching of scientific satellites. Injection point 29.7 N, 145.8 E .