L-6.55

Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

Notional LOx/Kerosene rocket engine. Study 1963. Engines used in recoverable stage of ballistic shape; separation at 3,420 m/s at 93,900 m altitude; splashdown using retrorockets under 7 parachutes 1340 km downrange.

Country: USA
Launch Vehicles: Nova GD-J
Propellants: Lox/Kerosene
Stages: Nova GD-J-1

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