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MR-125
LLNL solid rocket engine. Astrid first stage.

AKA: Astrid-1. Status: Retired 1994. Thrust: 400 N (80 lbf). Gross mass: 20 kg (44 lb). Unfuelled mass: 8.00 kg (17.60 lb). Burn time: 30 s. Height: 1.90 m (6.20 ft). Diameter: 0.17 m (0.55 ft).

Country: USA. Launch Vehicles: Astrid test vehicle. Propellants: Solid. Stages: MR-125. Agency: Livermore.
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