Experimental researches of possible low-thrust rocket adaptation developed by FSUE R&DIME for bipropellant MON-3+MMH providing tolerable thermal state thrusters

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Abstract

This paper gives firing test results comparison of FSUE R&DIME’s thrusters with the MON-3/MMH propellants and AT/UDMH propellants and also thruster thermal state information obtained during that firing testing.

About the authors

Yu. A. Beshenev

Research and Development Institute of Mechanical Engineering, Nizhnyaya Salda

Author for correspondence.
Email: niimash@list.ru
Chief Specialist of Thruster Development Russian Federation

S. A. Buldashev

Federal State Unitary Enterprise Research & Development Institute of Mechanical Engineering (R&DIME), Nizhnyaya Salda

Email: niimash@list.ru
Head of Design-Engineering Department Russian Federation

F. A. Kazankin

Federal State Unitary Enterprise Research & Development Institute of Mechanical Engineering (R&DIME), Nizhnyaya Salda

Email: niimash@list.ru
Deputy of Chief Designer Russian Federation

N. V. Lemskiy

Federal State Unitary Enterprise Research & Development Institute of Mechanical Engineering (R&DIME), Nizhnyaya Salda

Email: lemskii@mail.ru
Design Engineer of Design-Engineering Department Russian Federation

Ye. V. Semkin

Federal State Unitary Enterprise Research & Development Institute of Mechanical Engineering (R&DIME), Nizhnyaya Salda

Email: sewa20-68@rambler.ru
Head of Group of Design-engineering Department Russian Federation

References

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