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SS-520
Part of S-520
Japanese test vehicle. The SS-520 was a two-stage rocket, the first stage consisting of the main booster of the S-520. It had a capability of launching a 140 kg payload to an altitude of about 1,000 km, and with addition of a third stage, as a satellite launch vehicle.
Status: Active. First Launch: 1998-02-05. Last Launch: 2018-02-03. Number: 4 . Gross mass: 2,600 kg (5,700 lb). Height: 9.70 m (31.80 ft). Diameter: 0.52 m (1.70 ft). Apogee: 1,000 km (600 mi).
The SS-520 was a two-stage rocket, the first stage consisting of the main booster of the S-520. It had a capability of launching a 140 kg payload to an altitude of about 1,000 km.
Family:
test vehicle.
Country:
Japan.
Launch Vehicles:
S-520.
Launch Sites:
Kagoshima,
Kagoshima L,
SvalRak.
Stages:
SS-520 engine.
Agency:
Nissan.
1998 February 5 - .
08:30 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima L.
Launch Pad: K.
LV Family:
S-520.
Launch Vehicle:
SS-520.
- ENA / EPS / LAP Test / plasma mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 750 km (460 mi).
2000 December 4 - .
09:16 GMT - .
Launch Site:
SvalRak.
LV Family:
S-520.
Launch Vehicle:
SS-520.
- Ionosphere mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 1,108 km (688 mi).
2017 January 14 - .
23:33 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Kagoshima K.
LV Family:
S-520.
Launch Vehicle:
SS-520.
- TRICOM-1 - .
Nation: Japan.
Class: Technology.
Type: Technology satellite. Spacecraft: Cubesat.
COSPAR: 2017-0F01. Apogee: 200 km (120 mi). Perigee: -6,340 km (-6,340 mi). Inclination: 30.00 deg.
See TRICOM 1. Japan attempted to launch a single cubesat into orbit with a launch vehicle massing less than 3 tonnes. The SS-520 sounding rocket was furnished with a 78 kg third stage which was intended to orbit a 3U, 3 kg cubesat, TRICOM-1. The mission was flight SS-520-4 (SS-520-1 and 2 were normal sounding rocket flights; 3 has not yet flown.) However, telemetry was lost 20 seconds into flight, during first stage burn. Following range safety rules, the command to ignite stage 2 was not sent and the vehicle flew a suborbital path to about 200 km altitude and then splashed down in the ocean. The record smallest successful orbital launch vehicle remains the 9.4-tonne Lambda 4S, also Japanese,
which was retired in 1979.
2018 February 3 - .
05:03 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima K.
LV Family:
S-520.
Launch Vehicle:
SS-520.
- Tasuki - .
Payload: TRICOM-1R; TRICOM-1R (TASUKI). Nation: Japan.
USAF Sat Cat: 43201 . COSPAR: 2018-016A. Apogee: 256 km (159 mi). Perigee: 143 km (88 mi). Inclination: 30.94 deg. Period: 88.48 min. See TRICOM 1R (Tasuki). ..
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