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RM-3141


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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 RM-3141 GCR solid rocket engine. Jaguar third stage.

AKA: Jaguar-3. Status: Retired 1961. Thrust: 8.60 kN (1,933 lbf). Gross mass: 25 kg (55 lb). Unfuelled mass: 4.00 kg (8.80 lb). Burn time: 7.60 s. Height: 1.20 m (3.90 ft). Diameter: 0.15 m (0.49 ft).

Country: USA. Launch Vehicles: ASCAMP, Strongarm, Jaguar B-57. Propellants: Solid. Stages: RM-3141. Agency: JPL, GCR. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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