Sentence examples for propellant engine from inspiring English sources
They include a design for a new liquid oxygen-ethanol propellant engine and replacement of guidance systems for several surface-to-air missiles.
This paper presents a frameless eddy current sensor for cryogenic displacement measurement, for instance, the monitoring of axial displacement in liquid propellant engine.
The Optimal operation point of the system, and simultaneously the subsystems of a particular pump fed system in a cryogenic liquid propellant engine are determined by a hybridized optimization method.
The control strategy is realized in a number of loops, as long as the on and off modes of the propellant engine are focused on the Euler angles control, in finite burn time, and quaternion vector control, in non-burn time, respectively, in line with parameters variations.
In a word, the subject behind the research is to guarantee the desirable performance of a class of the autonomous space systems, which can be considered through the moments of inertia, the central of mass, the profile of the thrust vector and the misalignments of the propellant engine to deal with mission operation plans.
The spacecraft was equipped with a liquid propellant engine to perform rendezvous, and to reboost the space station.
Finally, cryogenic propellant engines and cryogenic propellant depots are briefly examined to show how cryogenic fluid management devices are required inside the propellant tank, particularly propellant management devices.
A new single range controller design approach for use with nonlinear liquid propellant engines (LPE) is developed.
Experiments were designed to simulate the dry-deposition of Mars soils onto spacecraft surfaces during an active descent landing scenario with propellant engines.
A new systematic single-range controller synthesis procedure for use with nonlinear, multivariable, and time-varying liquid propellant engines is developed.
The liquid-propellant engine itself consists of a main chamber for mixing and burning the fuel and oxidizer, with the fore end occupied by fuel and oxidizer manifolds and injectors and the aft end composed of the supersonic nozzle.
