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RH-560 engine


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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-560 engine ISRO/Antrix solid rocket engine. RH-560B second stage.

AKA: RH-560;RH-560B-2. Status: Retired 1998. Number: 1 . Thrust: 76.00 kN (17,085 lbf). Gross mass: 900 kg (1,980 lb). Unfuelled mass: 277 kg (610 lb). Burn time: 19 s. Height: 3.90 m (12.70 ft). Diameter: 0.56 m (1.83 ft).

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