Study on Cooling Characteristics of Mixed Gases with Hot Gas of Liquid Rocket Engine and Injected Liquid Nitrogen

Transactions of the Korean Society of Mechanical Engineers B ◽

10.3795/ksme-b.2012.36.10.1001 ◽

2012 ◽

Vol 36 (10) ◽

pp. 1001-1009

Author(s):

Jun-Su Jeon ◽

I-Sang Yu ◽

Joong-Il Kim ◽

Jai-Ho Kim ◽

Young-Sung Ko

Keyword(s):

Liquid Nitrogen ◽

Rocket Engine ◽

Liquid Rocket Engine ◽

Hot Gas ◽

Liquid Rocket ◽

Download Full-text

Hot-gas-side and coolant-side heat transfer in liquid rocket engine combustors

Journal of Thermophysics and Heat Transfer ◽

10.2514/3.574 ◽

1994 ◽

Vol 8 (3) ◽

pp. 524-530 ◽

Author(s):

Ten-See Wang ◽

Van Luong

Keyword(s):

Heat Transfer ◽

Rocket Engine ◽

Liquid Rocket Engine ◽

Hot Gas ◽

Download Full-text

Numerical analysis of the hot-gas-side and coolant-side heat transfer in liquid rocket engine combustors

10.2514/6.1992-3151 ◽

1992 ◽

Author(s):

TEN-SEE WANG ◽

LUONG VAN

Keyword(s):

Heat Transfer ◽

Numerical Analysis ◽

Rocket Engine ◽

Liquid Rocket Engine ◽

Hot Gas ◽

Download Full-text

The advanced liquid rocket engine line of SDO “Yuzhnoye” for the creation of new families of launch vehicles

Kosmìčna nauka ì tehnologìâ ◽

10.15407/knit2015.05.028 ◽

2015 ◽

Vol 21 (5(96)) ◽

pp. 28-35

Author(s):

А.А. Prokopchuk ◽

◽

V.А. Shulga ◽

Keyword(s):

Rocket Engine ◽

Liquid Rocket Engine ◽

Launch Vehicles ◽

The Creation ◽

Download Full-text

NUMERICAL SIMULATIONS ON THE COOLING JACKET CHANNEL OF A REGENERATIVELY COOLED LIQUID ROCKET ENGINE

Proceeding of Proceedings of CHT-17 ICHMT International Symposium on Advances in Computational Heat Transfer May 28-June 1, 2017, Napoli, Italy ◽

10.1615/ichmt.2017.330 ◽

2017 ◽

Author(s):

Daniele Ricci ◽

Francesco Battista ◽

Pasquale Natale ◽

Manrico Fragiacomo

Keyword(s):

Numerical Simulations ◽

Rocket Engine ◽

Liquid Rocket Engine ◽

Cooling Jacket ◽

Download Full-text

Mechanical Disturbances Arising From Thermal Power Deposition in a Gas with Application to Supercritical Liquid Rocket Engine Combustion Instability

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ◽

10.2514/6.2013-567 ◽

2013 ◽

Author(s):

David Kassoy

Keyword(s):

Rocket Engine ◽

Thermal Power ◽

Combustion Instability ◽

Liquid Rocket Engine ◽

Power Deposition ◽

Engine Combustion ◽

Liquid Rocket ◽

Mechanical Disturbances

Download Full-text

INFLUENCE OF FILLING PROCESSES FOR MIXING HEAD OF GAS GENERATORS ON DYNAMICS OF LIQUID ROCKET ENGINE WITHOUT STARTER DEVICE

Siberian Journal of Science and Technology ◽

10.31772/2587-6066-2018-19-3-469-481 ◽

2018 ◽

Vol 19 (3) ◽

pp. 469-481

Author(s):

E.N. Belayev ◽

◽

A.G. Vorobyev ◽

Keyword(s):

Rocket Engine ◽

Liquid Rocket Engine ◽

Gas Generators ◽

Download Full-text

Unsteady Side-Load Evolution in a Liquid Rocket Engine Nozzle

Journal of Spacecraft and Rockets ◽

10.2514/1.a34556 ◽

2020 ◽

Vol 57 (2) ◽

pp. 391-397

Author(s):

S. B. Verma ◽

Oskar Haidn

Keyword(s):

Rocket Engine ◽

Liquid Rocket Engine ◽

Side Load ◽

Download Full-text

Overview and analysis of the experimentally measured throat heat transfer in liquid rocket engine thrust chambers

Acta Astronautica ◽

10.1016/j.actaastro.2021.03.028 ◽

2021 ◽

Vol 184 ◽

pp. 46-58

Author(s):

Marco Pizzarelli

Keyword(s):

Heat Transfer ◽

Rocket Engine ◽

Liquid Rocket Engine ◽

Engine Thrust ◽

Download Full-text

Rotordynamic analysis of a high thrust liquid rocket engine fuel (Kerosene) turbopump

Aerospace Science and Technology ◽

10.1016/j.ast.2012.03.005 ◽

2013 ◽

Vol 26 (1) ◽

pp. 169-175 ◽

Author(s):

Seong Min Jeon ◽

Hyun Duck Kwak ◽

Suk Hwan Yoon ◽

Jinhan Kim

Keyword(s):

Rocket Engine ◽

Liquid Rocket Engine ◽

Engine Fuel ◽

Liquid Rocket ◽

Download Full-text

Measurements of Rotordynamic Coefficients of Hybrid Bearings With (a) a Plugged Orifice, and (b) a Worn Land Surface

Journal of Engineering for Gas Turbines and Power ◽

10.1115/1.1403461 ◽

2002 ◽

Vol 124 (2) ◽

pp. 363-368 ◽

Author(s):

F. Laurant ◽

D. W. Childs

Keyword(s):

Test Data ◽

Land Surface ◽

Rocket Engine ◽

Liquid Rocket Engine ◽

Test Results ◽

Rotordynamic Coefficients ◽

Hybrid Bearing ◽

Test results are presented for the rotordynamic coefficients of a hybrid bearing that is representative of bearings for liquid-rocket-engine turbopump applications. The bearing is tested in the following two degraded conditions: (a) one of five orifices plugged, and (b) a locally enlarged clearance to simulate a worn condition. Test data are presented at 24,600 rpm, with supply pressures of 4.0, 5.5, and 7.0 MPa, and eccentricity ratios from 0.1 to 0.5 in 0.1 increments. Overall, the results suggest that neither a single plugged orifice nor significant wear on the bearing land will “disable” a well-designed hybrid bearing. These results do not speak to multiple plugged orifices and are not an endorsement for operations without filters to prevent plugging orifices.

Download Full-text