Search by keyword: chamber coefficient | Engineering Journal: Science and Innovation

Search by keyword: "chamber coefficient"

Computational study of the thermal state of a low-thrust rocket engine chamber operating on the gaseous propellant components taking into account the axial heat leaks along the combustion chamber fire wall

Published: 23.06.2025

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #6(162)/2025

DOI:

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Computational study of the thermal state of a low-thrust rocket engine chamber operating on the gaseous propellant components taking into account the axial heat leaks along the combustion chamber fire wall

Published: 23.06.2025

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #6(162)/2025

DOI:

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Computation study of the low-thrust rocket engine chamber thermal state operating on the oxygen + methane gaseous propellant components with the structural elements regenerative external cooling by an oxidizer

Published: 01.11.2024

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #11(155)/2024

DOI: 10.18698/2308-6033-2024-11-2402

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Computation study of the low-thrust rocket engine chamber thermal state operating on the oxygen + methane gaseous propellant components with the structural elements regenerative external cooling by an oxidizer

Published: 01.11.2024

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #11(155)/2024

DOI: 10.18698/2308-6033-2024-11-2402

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Computational study of the various mixture formation schemes and determination of the main factors influencing the working process parameters of the low-thrust rocket engine combustion chamber

Published: 07.12.2023

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #12(144)/2023

DOI: 10.18698/2308-6033-2023-12-2325

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Computational study of the various mixture formation schemes and determination of the main factors influencing the working process parameters of the low-thrust rocket engine combustion chamber

Published: 07.12.2023

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #12(144)/2023

DOI: 10.18698/2308-6033-2023-12-2325

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Computational studies to optimize the geometry of the low-thrust rocket combustion chamber using gaseous propellants

Published: 24.11.2021

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #11(119)/2021

DOI: 10.18698/2308-6033-2021-11-2129

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Parametric study of the effect of mode and geometric factors on the chamber coefficient of a liquid-propellant engine with a slotted nozzle head

Published: 09.04.2021

Authors: Novikov A.V., Andreev E.A.

Published in issue: #4(112)/2021

DOI: 10.18698/2308-6033-2021-4-2071

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts