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RH-300
Part of RH
Indian single stage sounding rocket. Sounding rocket derived from French Belier rocket engine technology.
Status: Active. First Launch: 1975-01-01. Last Launch: 1999-11-01. Number: 10 . Thrust: 38.00 kN (8,542 lbf). Gross mass: 300 kg (660 lb). Height: 4.10 m (13.40 ft). Diameter: 0.31 m (1.01 ft). Apogee: 150 km (90 mi).
Subtopics
| RH-300-II ISRO solid rocket engine. RH-300 Mk II first stage. |
Country:
India.
Launch Sites:
Thumba Pad 5.
Stages:
RH-300 engine.
Agency:
ISRO.
1975 - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-300.
- First Flight test - .
Nation: India.
Agency: ISRO.
Apogee: 130 km (80 mi).
1978 April 18 - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-300.
- AST 1 Technology mission - .
Nation: India.
Agency: ISRO.
Apogee: 130 km (80 mi).
1979 August 25 - .
06:21 GMT - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-300.
- ISRO-CNES I Ionosphere mission - .
Nation: India.
Agency: ISRO.
Apogee: 150 km (90 mi).
1979 August 31 - .
05:51 GMT - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-300.
- ISRO-CNES II Ionosphere mission - .
Nation: India.
Agency: ISRO.
Apogee: 150 km (90 mi).
1986 March 10 - .
04:55 GMT - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-300.
- D-region ionization comparison Aeronomy mission - .
Nation: India.
Agency: ISRO.
Apogee: 110 km (60 mi).
1986 October 1 - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-300.
- AEROSOL PRECAMP. II Aeronomy mission - .
Nation: India.
Agency: ISRO.
Apogee: 100 km (60 mi).
1986 October 3 - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-300.
- AEROSOL PRECAMP. II Aeronomy mission - .
Nation: India.
Agency: ISRO.
Apogee: 100 km (60 mi).
1993 - .
Launch Site:
Thumba.
Launch Complex:
Thumba Pad 5.
LV Family:
RH.
Launch Vehicle:
RH-300.
- Ionosphere mission - .
Nation: India.
Agency: ISRO.
Apogee: 100 km (60 mi).
1993 - .
Launch Site:
Thumba.
Launch Complex:
Thumba Pad 5.
LV Family:
RH.
Launch Vehicle:
RH-300.
- Ionosphere mission - .
Nation: India.
Agency: ISRO.
Apogee: 100 km (60 mi).
1999 November 1 - .
Launch Site:
Sriharikota.
LV Family:
RH.
Launch Vehicle:
RH-300.
- EWS? Ionosphere mission - .
Nation: India.
Agency: ISRO.
Apogee: 135 km (83 mi).
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