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XM-45
Rocket solid engine. Trailblazer 2 M second stage.

AKA: Trailblazer 2 M-2. Status: Retired 1966. Thrust: 200.00 kN (44,960 lbf). Gross mass: 900 kg (1,980 lb). Unfuelled mass: 377 kg (831 lb). Burn time: 6.00 s. Height: 4.50 m (14.70 ft). Diameter: 0.38 m (1.24 ft).



Country: USA. Launch Vehicles: RAM A, HJ PRV. Propellants: Solid. Stages: XM-45.

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