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RH-125


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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-125 Part of RH Indian ISRO VSSC sounding rocket. Single stage vehicle

Status: Retired 1971. First Launch: 1970-01-01. Last Launch: 1971-10-09. Number: 2 . Thrust: 8.40 kN (1,888 lbf). Gross mass: 20 kg (44 lb). Unfuelled mass: 11 kg (24 lb). Burn time: 2.90 s. Height: 2.50 m (8.20 ft). Diameter: 0.12 m (0.39 ft). Apogee: 20 km (12 mi).

Subtopics RH-125S ISRO VSSC solid rocket engine. Menaka II second stage. Country: India. Launch Vehicles: Menaka II, RH-125, RH-200. Propellants: Solid. Launch Sites: Thumba, Sriharikota. Agency: ISRO. 1970 - . Launch Site: Thumba. LV Family: RH. Launch Vehicle: RH-125. 1971 October 9 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-125. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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