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

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

Russian Federation Chief Specialist of Thruster Development

S. A. Buldashev

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

Email: niimash@list.ru

Russian Federation Head of Design-Engineering Department

F. A. Kazankin

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

Email: niimash@list.ru

Russian Federation Deputy of Chief Designer

N. V. Lemskiy

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

Email: lemskii@mail.ru

Russian Federation Design Engineer of Design-Engineering Department

Ye. V. Semkin

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

Email: sewa20-68@rambler.ru

Russian Federation Head of Group of Design-engineering Department

References

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