thrust output

thrust output

[′thrəst ′au̇t‚pu̇t]
(aerospace engineering)
The net thrust delivered by a jet engine, rocket engine, or rocket motor.
References in periodicals archive ?
Developed by Keppel's design arm, Marine Technology Development, DLV 2000 is capable of achieving efficient pipelay rates for long trunklines and operating in severe weather conditions while maintaining significant thrust output and power distribution.
To achieve the requested thrust output the design utilizes a mass flow sensor for real-time measurements of the gas flow in the feedback signal of the control loop of the flow control valve.
However, proportional thrust regulation would in principle increase the orbit keeping time as the thrust output could be adjusted according to variations in the atmospheric drag.
GE has already increased the thrust output the engine has to produce and more changes may still come, he added.
A high expansion ratio leads to low exhaust pressure, increasing the conversion of potential output (represented by the chamber temperature and pressure) to thrust output (exhaust momentum and pressure).
Thrust output (in pounds) is given by the expression: F=2[pi]peNT, where p = drivescrew pitch (rev/in); e = drivetrain efficiency; N = reducer ratio; and T = input torque (lb-in).
In fact, we have already defined the engine growth steps to achieve a 25% increase in thrust output in preparation for meeting future customer requirements.
It is also capable of achieving efficient pipe lay rates for long trunk lines, operating in severe weather conditions, and providing significant thrust output and power distribution.
Higher torque and thrust outputs also can be provided.