S-210
Launch vehicle · Japan
Original archive entry. The text, images and links below are kept as they were written.
Japanese ISAS sounding rocket. Single stage ionospheric sounding rocket used for research from Japan's Antarctic base.
The S-210 (S for single stage; 210 for 210 mm diameter) rocket was designed for low-cost observations of the ionosphere above 100 km altitude. The S-160 sub-scale version of the rocket proved the design concepts. The first two launches of the full sized versions in 1966-1967, .PT-210-1 and -2, were failures, with the motor case burning through. After redesign of the case and improved quality control, S-210-1 and -2 were successfully launched in August 1969. Following further successful tests in Japan in 1970-1971, the rocket was cleared for intensive use at the Japanese Antarctic base at Syowa in 1972-1978.
The rocket motor used butadiene propellant, which has good low temperature properties suited for use at the South Pole. The tapered circular grain provided 17 seconds of thrust. The combustion chamber was of chrome molybdenum steel, protected by a phenol resin-quartz glass fiber ablative covering. Stabilization was by a spin motor that produced 2 revolutions-per-second.
Subtopics
- TT-210 engine NASDA solid rocket engine. TT-210 first stage.
Related
- Country
- Japan
- Propellants
- Solid
- Launch Sites
- Kagoshima, Syowa Base
Chronology
47 events
1966 August 6
06:30 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1967 March 11
06:30 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1969 August 7
Launch Site: Kagoshima. Launch Vehicle: S-210.1969 August 8
12:00 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1970 January 17
01:20 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1970 September 28
01:20 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1971 January 16
02:00 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1971 June 24
01:05 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1971 July 21
21:52 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1971 August 10
02:24 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1971 September 13
21:50 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1971 September 24
21:08 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1971 December 3
12:00 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1972 January 21
02:24 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1972 January 29
Launch Site: Kagoshima. Launch Vehicle: S-210.1972 February 11
12:00 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1972 February 17
08:00 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1972 May 13
23:13 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1972 May 15
23:02 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1972 August 7
01:45 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1972 August 11
01:01 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1972 December 13
21:23 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1973 January 15
23:40 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1973 February 14
20:45 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1973 March 25
17:47 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1973 April 22
18:25 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1973 June 10
17:20 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1973 June 11
18:10 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1973 July 15
16:09 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1973 August 19
09:55 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.1973 August 22
21:53 GMT - . Launch Site: Syowa Base. Launch Vehicle: S-210.1974 August 20
09:55 GMT - . Launch Site: Kagoshima. Launch Vehicle: S-210.- NNP / NEL / TEL Aeronomy / ionosphere mission - . Nation: Japan. Agency: ISAS. Apogee: 112 km (69 mi).