Method whereby sloshing stability of booster, with arbitrary number of fuel tanks, may be determined by inspection; means of eliminating slosh instability by employing accelerometer feedback is investigated; scheme has advantage of reducing weight penalty incurred by use of baffles to damp sloshing motion; rational determination of parameters previously obtained by computer simulation is possible.
Analysis of liquid-propellant mode stability of multitank ballistic booster vehicle
J Aerospace Sciences
Journal of the Aero/Space Sciences ; 29 , n 2
1962
10 pages
Aufsatz (Zeitschrift)
Englisch
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