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S-4 engine
Part of LR105
Rocketdyne LOx/Kerosene rocket engine. Design ca. 1957. Version of Atlas sustainer tailored to Redstone Arsenal upper-stage requirements. Paper study only. Used on Super Jupiter launch vehicle.
AKA
: S-4.
Status
: Design ca. 1957.
Date
: 1957.
Thrust
: 412.80 kN (92,801 lbf).
Country
:
USA
.
Launch Vehicles
:
Super-Jupiter
.
Propellants
:
Lox/Kerosene
.
Stages
:
Super-Jupiter-3
.
Agency
:
Rocketdyne
.
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