默林火箭发动机
参考资料

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1 2 3 4  Mueller, Thomas. . 2015-06-08  [2015-07-09]. The Merlin 1D weighs 1030 pounds, including the hydraulic steering (TVC) actuators.  It makes 162,500 pounds of thrust in vacuum.  that is nearly 158 thrust/weight.  The new full thrust variant weighs the same and makes about 185,500 lbs force in vacuum.
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↑  Bergin, Chris. . NASA Spaceflight.com. 2012-01-11  [2012-12-28]. （原始内容存档于2017-01-18）. – Increased reliability: Simplified design by eliminating components and sub-assemblies. Increased fatigue life. Increased chamber and nozzle thermal margins,” noted SpaceX in listing the improvements in work. – Improved Performance: Thrust increased from 95,000 lbf (sea level) to 140,000 lbf (sea level). Added throttle capability for range from 70-100 percent. Currently, it is necessary to shut off two engines during ascent. The Merlin 1D will make it possible to throttle all engines. Structure was removed from the engine to make it lighter. – Improved Manufacturability: Simplified design to use lower cost manufacturing techniques. Reduced touch labor and parts count. Increased in-house production at SpaceX.
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↑  . MICROMO/Faulhabler. 2015  [2015-08-14]. （原始内容存档于2017-02-20）. the fuel-trim valve adjusts the mixture in real time.  The fuel-trim device consists of a servo-motor-controlled butterfly valve. To achieve the proper speed and torque, the design incorporates a planetary gearbox for a roughly 151:1 reduction ratio, gearing internal to the unit. The shaft of the motor interfaces with the valve directly to make fine adjustments. 'The basic mixture ratio is given by the sizing of the tubes, and a small amount of the flow of each one gets trimmed out,' explains Frefel. 'We only adjust a fraction of the whole fuel flow.'
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SpaceX默林1A 发动机
SpaceX工厂里正在建造的Merlin 1C