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Experimental researches of possible low-thrust rocket adaptation developed by FSUE R&DIME for bipropellant MON-3+MMH providing tolerable thermal state thrusters
- Authors: Beshenev Y.A.1, Buldashev S.A.2, Kazankin F.A.2, Lemskiy N.V.2, Semkin Y.V.2
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Affiliations:
- Research and Development Institute of Mechanical Engineering, Nizhnyaya Salda
- Federal State Unitary Enterprise Research & Development Institute of Mechanical Engineering (R&DIME), Nizhnyaya Salda
- Issue: Vol 10, No 3-1 (2011): Special Issue
- Pages: 267-270
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/1758
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-1(27)-267-270
- ID: 1758
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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
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