Review of atomization and mixing characteristics of pintle injectors

F Zhao, H Zhang, H Zhang, B Bai, L Zhao - Acta Astronautica, 2022 - Elsevier
To promote the design and optimization as well as a deeper understanding of pintle
injectors further, the progress on atomization and mixing characteristics of pintle injectors …

[PDF][PDF] Theoretical Aspects on Design and Performance Characteristics of solid rocket motor

AK Mishra, S Jadhav, M Akshay - International Journal of All …, 2022 - researchgate.net
ABSTRACT Solid Rocket Motors are widely used in sounding rockets and airborne missiles.
The main reason for the study in this field is that the solid rocket motor is very easy to handle …

[PDF][PDF] Theoretical and numerical investigation on propulsive configuration and performance characteristics for a sounding rocket

AK Mishra, VS Janani Kavipriya… - International Journal of …, 2022 - researchgate.net
This paper gives the overview of a sounding rocket which is developed to perform certain
scientific experiments in low earth orbit. The propulsion characteristics and calculations …

Analysis and optimization of Dual secondary fuel injector for Thrust vector control

K Sharma, P Manohar, AK Mishra - Journal of Physics …, 2022 - iopscience.iop.org
The motive of this analysis is to compare the performance parameters of a single secondary
fuel injector and performance of Dual Secondary fuel injector system for Thrust Vector …

Design, Manufacturing and Cold Flow Testing of a Liquid Rocket Engine 3D Printed Pintle Injector.

H Broomby, E Trifoni - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
Rocket engine design has a long heritage, however, only recently has it become accessible
beyond private industry with modern manufacturing techniques like additive metal …

[PDF][PDF] Chemical Rocket Motors for Space Launch Applications: Parametric Approach

JK VS, M Akshay, S Mane, SD Jadhav - 2022 - researchgate.net
Hybridrocket motors are widely used in heavy launch vehicles with maximum payload
capacity. The main reason for the study in this field is that the hybrid rocket motor is very …

[PDF][PDF] Material Selection for Space Launch Vehicles: Theoretical Perspective

JKP VS, P Thota, SD Jadhav - researchgate.net
Around the aerospace domain the featuring of advanced missiles and rockets results in
search of new and novel materials. We may employ newer and lighter materials in the …

[PDF][PDF] Theoretical Study on Film Cooling Process for Rocket Combustor

S Mane - researchgate.net
The definition of film cooling is combined with regenerative cooling which is an efficient way
to ensure the long term, safe and secure functioning of liquid rocket engines with higher heat …

[PDF][PDF] Effect of Area Ratio and Nozzle Pressure Ratio for CD Nozzle─ Short Review

S Mane, P Thota, Y Deshmukh, R Gupta - researchgate.net
ABSTRACT CD Nozzle plays a vital role for thrust optimization in rocket in order to carry it in
outer space. The exhaust velocity flowing out of nozzle represents to be the supersonic flow …

[PDF][PDF] Parametric flow study inside convergent-divergent nozzle using CFD method

S Mane, SD Jadhav, Y Deshmukh - researchgate.net
Computational fluid dynamics is a branch of fluid mechanics that deals with problems
related to fluid flow and solves numerical methods and algorithms. Computational methods …