1 The rocket engine burned out.

2 A comparison of different kinds of rocket engines with each other requires some measure of their performance.

3 This had never been done before with a rocket engine.

4 Turbopump is an important part in liquid rocket engine.

5 Mo nozzle for the rocket engine nozzle professional.

6 Milling grooves on aerospace rocket engine - nozzle surface is an important process.

7 The leak of Liquid Rocket Engine ( LRE ) is very common and dangerous.

8 Of course, the clouds were rocket engine plumes from the predawn launch of the space shuttle Discovery on the STS-131 mission to the International Space Station.

9 With a tremendous roar from its rocket engine, the satellite is sent up into the sky.

10 The BRABUS ROCKET engine and the entire drivetrain is operated high - performance lubricants from technology partner ARAL.

11 The expander cycle rocket engine could provide an ideal high energy and low - cost upper stage option.

12 The first native liquid-fueled rocket engine used a liquid oxygen and carbon-hydrogen propellant, provided 5.6 tons of thrust, and was installed in unit E.

13 The reliability of operational liquid rocket engine is closely related to the health monitoring technology.

14 Unlike a rocket engine , the jet engine , as you know, is an " air breather ".

15 For propulsion, it relies on the aerospike, a linear rocket engine.

16 By 1909 he was already aware of the superior potential of liquid hydrogen-liquid oxygen rocket engines.

17 It was placed in an eccentric, high-inclination orbit around Venus by the firing of a small rocket engine.

18 A mathematical model describing combustion in a high pressure liquid hypergolic bipropellant(UDMH/H2O4) rocket engine combustor has been developed.

19 The result of analysis provides a basis for the application of composite material on rocket engine.

20 Comes to the conclusion that the hybrid bearing can be used to the liquid rocket engine turbopump, and then puts forward the key technique to be solved.

21 Rotor dynamic is one of the most complicated problems in development of LOX turbopump of liquid rocket engine.

22 To analyze the reason of the three-stage engine turn-off delay of some liquid rocket engine, the stable state fault module of the engine was established in this paper.

23 Two accumulative error indices are defined as the discernment signals of the fault detection in a liquid propellant rocket engine.

24 The 90-metre-long craft's secret weapon is a hydrogen fuel-powered rocket engine called SABRE (Synergistic Air-Breathing Rocket Engine) and was designed by the company's managing director Alan Bond.

25 A new type gasdynamic arming switch of rocket base fuze was studied, which closes the electronic delay arming device utilizing the gas from rocket engine.

26 For one thing, they simplify the design of a rocket engine.

27 A new modular method is proposed for static simulation of liquid rocket engine.

28 Achieving that speed is possible thanks to the craft's specialized rocket engine, a hypersonic scramjet.

29 In preparation for the June 3 launch, Tycho Brahe is hoisted atop the HEAT-1X rocket engine in an undated picture.

30 Two-phase turbulent reacting flow model of the internal operating processes in Liquid Rocket Engine (LRE) is set up in non-orthogonal curvilinear coordinates.

31 The theoretical specific impulse formula for two-phase flow in nozzle of rocket-ramjet engine is derived on the basis of similarity to that used for rocket engine.

32 Seen from above, the spacecraft Tycho Brahe is settled onto the HEAT-1X rocket engine.

33 The integrity test of Liquid Rocket Engine ( LRE ) must be carried out before its launch.

34 Unlike a rocket engine , the jet engine , as you konw, is an " air breather ".

35 The research result has some reference values to rocket engine research institute building and strategy development.

36 This paper mainly discusses available structures of the liquid hybrid bearings and the key technologies that need to be solved for the liquid rocket engine turbopump .

37 In this paper, the extrapolation formulas of rocket engine performance parameters are established utilizing one isentropic reference line and two partial derivatives for fixed enthalpy.

38 Attributing to the large flow rate, high efficiency level reaction turbine is adoptive in staged combustion cycle liquid rocket engine.

39 Exhaust nozzle is one of the key components of pulse detonation rocket engine (PDRE). Exhaust nozzle can be used to improve the propulsion performance of PURE.

40 A gas flow model with laser plasma as heat source was developed based on axial symmetric Euler equations in the laser propulsion rocket engine absorption chamber.

41 To deal with the lack of fault samples in the fault detection of a Liquid Rocket Engine (LRE) turbopump , a detection model based on one-class support vector machines (OC-SVMs) was founded.

41 try its best to collect and create good sentences.

42 In the present study, we design an automatic remote control system, which is used to push the mandril out of large rocket engine.

43 Private spaceflight took one giant step forward this week when the Tycho Brahe craft lifted off atop the HEAT-1X rocket engine Friday (pictured) from a platform in the Baltic Sea.

44 The feed system of a rocket engine may be the cause of undesirable oscillations.

45 On the basis of the fault simulation for a liquid rocket engine and the statistical analysis for fire-test data in ground test, the major and important failure modes of the engine are summarized.

46 Disigning coolant channel on the firebox of liquid rocket engine to loxodrome(equal-angle helix) groove can improve firebox coolant capability greatly.

47 As to reliability growth management being an uncertain decision based on imperfect information, FMEA and fault diagnosis model have been built for liquid rocket engine.

48 Vacuum vessel seal structure used in the leak test of a liquid rocket engine turbopump is discussed.

49 In this paper, the fault status induced by rubbing between rotor and stator of liquid rocket engine turbopump system is analyzed.

50 A well-established way to get more energy from a gravity assist is to fire a rocket engine at periapsis where a spacecraft is at its maximum velocity.

51 The performance characteristics, structure and working cycle of pulse detonation rocket engine ( PDRE ) were introduced firstly.

52 This obturator can satisfy requirement of rocket engine on the interior ballistic and exterior ballistic.

53 And, oil painter Robert McCall imagines the sight of the rocket engine firing to propel the lunar lander back to earth.

54 The effect of the outer- volatilization of a rocket engine charge on the muzzle velocity was discussed and some ways and measures to guide manufacture were suggested.