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a rocket
Equations of motion of ball lightning in a rocket airstream
      
Phenomena accompanying the injection of a dense plasma beam from the payload of a rocket into ionospheric plasma are analyzed.
      
It has been indicated that a change in the total electron content is caused by the propagation of an acoustic gravity wave pulse, generated during a rocket flight along the horizontal trajectory leg, in the ionosphere.
      
The proposed model was successfully used to analyze two emergency events: a failure of a steam turbine's cast diaphragm and a failure of a rocket engine's oxygen pump booster stage.
      
Regenerative cooling is an advanced method which can ensure not only the proper running but also higher performance of a rocket engine.
      
This profile was chosen because of simplicity, but also of being similar to the one for a rocket inducer impeller.
      
A two-dimensional computational model of the dynamics of a radiating turbulent fireball that can form in accident-induced explosion of a rocket at the launching position or in flight is presented.
      
An apparatus for the measurement of X-rays from 25 to 200 keV was flown aboard a rocket.
      
The motion should be as that of a rocket emitting random bursts of jets with isotropic distribution and also subject to the external, deterministic forces.
      
A rocket immunoelectrophoresis (RIE) procedure was developed allowing the detection of even spurious contaminations with peanut protein.
      
Coresponding conclusions are drawn for a rocket type rod system.
      
An improved resonant fluorescence instrument for measuring atomic oxygen concentration was developed to avoid the Doppler effect and the aerodynamic shock effect due to the supersonic motion of a rocket.
      
Using the instrument, the altitude profile of atomic oxygen concentration was observed by a rocket experiment at Uchinoura (31°N) on 28 January 1992.
      
In 1997, reliable operation of the EISCAT Svalbard Radar (ESR) was achieved and a rocket launching facility at Ny ?lesund on Svalbard (79°N, 12°E) (SVALRAK) was established.
      
Since solid propellant material is of viscoelastic behaviour an approximate viscoelastic solution methodology for the multilayered shell is described for estimation of time dependent solutions of propellant grain in a rocket motor.
      
On 17th and 22nd March, 1951, the measurements of the decrease in the earth's magnetic field were continued by means of a magnetometer set up in a rocket.
      
Anticipated reduction in cost of hydrazine, resulting from its increased production as a rocket fuel, suggests the need to reconsider this chemical as an industrial reactant for fats.
      
This creates a "rocket" effect with the potential to cause serious personal injury and/or property damage.
      
We present a case of an allied soldier who was accidentally shot from a very close range on his right thigh by a rocket-propelled grenade (RPG).
      
This interferometer has been successfully flown on a rocket and obtained measurements of atmospheric limb emission at tangent altitudes from 70 km to 150 km.
      
 

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