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RH-300-II


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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-II Part of RH-300 ISRO solid rocket engine. RH-300 Mk II first stage.

AKA: RH-300 Mk II-1. Status: Active. Thrust: 39.10 kN (8,790 lbf). Gross mass: 500 kg (1,100 lb). Burn time: 20 s. Height: 3.40 m (11.10 ft). Diameter: 0.31 m (1.01 ft).

Country: India. Launch Vehicles: RH-300 Mk II, RH-560/300 Mk II. Propellants: Solid. Stages: RH-300-II. Agency: ISRO. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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