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Laboratory Simulation of the Effect of Rocket Thrust on a Precessing Space Vehicle

Laboratory Simulation of the Effect of Rocket Thrust on a Precessing Space Vehicle

          
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About the Book

Ground tests of solid propellant rocket motors have shown that metal-containing propellants produce various amounts of slag (primarily aluminum oxide) which is trapped in the motor case, causing a loss of specific impulse. Although not yet definitely established, the presence of a liquid pool of slag also may contribute to nutational instabilities that have been observed with certain spin-stabilized, upper-stage vehicles. Because of the rocket's axial acceleration, absent in the ground tests, estimates of in-flight slag mass have been very uncertain. Yet such estimates are needed to determine the magnitude of the control authority of the systems required for eliminating the instability. A test rig with an eccentrically mounted hemispherical bowl was designed and built which incorporates a follower force that properly aligns the thrust vector along the axis of spin. A program that computes the motion of a point mass in the spinning and precessing bowl was written. Using various RPMs, friction factors, and initial starting conditions, plots were generated showing the trace of the point mass around the inside of the fuel tank. The apparatus will incorporate future design features such as a variable nutation angle and a film height measuring instrument. Data obtained on the nutational instability characteristics will be used to determine order of magnitude estimates of control authority needed to minimize the sloshing effect. Alvarez, Oscar and Bausley, Henry and Cohen, Sam and Falcon-Martin, Miguel and Furumoto, Gary (Editor) and Horio, Asikin and Levitt, David and Walsh, Amy Unspecified Center ALUMINUM OXIDES; FUEL TANKS; GROUND TESTS; LIQUID SLOSHING; NUTATION; PROPELLANTS; ROCKET THRUST; SIMULATION; SLAGS; SOLID PROPELLANT ROCKET ENGINES; ESTIMATES; FRICTION FACTOR; LOSSES; MEASURING INSTRUMENTS; SPECIFIC IMPULSE; STABILITY...


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Product Details
  • ISBN-13: 9781731186188
  • Publisher: Independently Published
  • Publisher Imprint: Independently Published
  • Height: 280 mm
  • No of Pages: 120
  • Spine Width: 6 mm
  • Width: 216 mm
  • ISBN-10: 1731186185
  • Publisher Date: 12 Nov 2018
  • Binding: Paperback
  • Language: English
  • Returnable: N
  • Weight: 294 gr


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