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Calculation of initial dynamically unstabilized sections in the elements of liquid rocket engines turbopump units
Calculation of initial dynamically unstabilized sections in the elements of liquid rocket engines turbopump units
2021
A. A. Zuev
A. A. Arngold
V. P. Nazarov
V N Mehtieva
E V Khodenkova
Keywords:
Aerospace engineering
Materials science
Liquid-propellant rocket
Turbopump
Correction
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