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Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing
- Authors: Nigodjuk V.E.1, Sulinov A.V.1
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Affiliations:
- Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
- Issue: Vol 10, No 3-3 (2011): Special Issue
- Pages: 265-268
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6890
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-3(27)-265-268
- ID: 6890
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Abstract
As a result of theoretical and experimental studies have shown that the main reason for the low efficiency of two-component liquid-propellant thrusters (0.1 ... 1) N on hypergolic propellants with jet mixing scheme is the low efficiency of liquid-phase mixing of the components. Proposed and experimentally investigated a method for increasing the energy efficiency of two-component liquid-propellant thrusters (0,1 ... 1) N on hypergolic propellants with jet mixing scheme due to the intensification of liquid-phase mixing of the components with predkamernogo device.
About the authors
V. E. Nigodjuk
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Author for correspondence.
Email: ke_src@ssau.ru
candidate of technical science, associate professor
Russian FederationA. V. Sulinov
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Email: ke_src@ssau.ru
candidate of technical science, associate professor
Russian FederationReferences
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