SEPR 2

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SEPR 2

SEPR rocket engine. SE 4100 SAM. Used turbopumps SEPR 3 and SEPR 4. First flight 1950.

AKA: SE.4100. Date: 1950-1951. Thrust: 1,250.00 kN (281,010 lbf).

Family: Storable liquid. Country: France. Launch Vehicles: SE.4100. Agency: SEPR.

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