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MARC 13A1
ARC solid rocket engine. Hydra-Iris first stage.

AKA: Hydra-Iris-1. Status: Retired 1968. Thrust: 17.00 kN (3,821 lbf). Gross mass: 500 kg (1,100 lb). Unfuelled mass: 112 kg (246 lb). Burn time: 52 s. Height: 4.00 m (13.10 ft). Diameter: 0.30 m (0.98 ft).



Country: USA. Launch Vehicles: Iris, Hydra-Iris. Propellants: Solid. Stages: MARC 13A1. Agency: Atlantic Research.

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