H-1 engine cut-off sequence |
H-1 engines for the S-IB booster stage |
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The eight H-1 engines at the base of the S-IB stage. These pictures were taken in the final assembly area of Michoud Assembly Facility (MAF) near New Orleans.
Scanning credit to Kipp Teague |
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H-1 engine |
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Technical drawings of the H-1 engine.
The highlighted components are mentioned in the explanation of the H-1 ignition sequence below. The H-1 produced about 91 metric Tons of thrust. Eight of these engines were used to lift the 590 metric Tons heavy Saturn IB from the launch pad.
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The cut-off sequence boils down to only one step: close the Main LOX valve to stop the combustion in the thrust chamber and the combustion chamber of the gas generator (LPGG).
The Main Fuel Valve (MLV) remains open to allow for a fuel-rich cut-off. |
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START OF CUT-OFF SEQUENCE
A cut-off signal is sent to the Conax valve to activate explosive actuators to provide closing pressure to the control port of the Main LOX Valve. |
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CUT-OFF FROM LOX SUPPLY COMBUSTION IS STOPPED The LOX supply is cut-off first. This allows for a fuel-rich cut-off.
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CUT-OFF FROM FUEL SUPPLY
The fuel / hydraulic pressure on the control port of the Main Fuel Valve (MFV) has dropped below 10 atm. The MFV closes. |
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