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RH-300
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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z 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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