RX-320 Rocket Static Pressure Combustion Chamber Prediction and Validation by Using Invers Method

Jurnal Teknologi Dirgantara
doi 10.30536/j.jtd.2018.v16.a2866
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Indonesian National Institute of Aeronautics and Space (LAPAN)

Related search

Development of PM Concentration Measurement at Combustion Chamber Outlet by Using Laser Measuring Method.

Journal of The Japan Institute of Marine Engineering
2001English

Increasing the Specific Impulse of Liquid Oxygen + Kerosene Rocket Engines by Introducing Hydrogen Into the Combustion Chamber

Engineering Journal: Science and Innovation
2019English

Evaluation of Combustion Chamber Design Using CFD

MM Science Journal
Electronic EngineeringIndustrialMechanical EngineeringAutomotive EngineeringManufacturing EngineeringElectrical
2019English

Aluminized Composite Solid Propellant Particle Path in the Combustion Chamber of a Solid Rocket Motor

WIT Transactions on Engineering Sciences
Mechanics of MaterialsElectronic EngineeringMechanical EngineeringMaterials ScienceFluid FlowElectrochemistryTransfer ProcessesElectricalComputational MechanicsMathematics
2006English

Recent Trend of Combustion Property of Marine Residual Fuel Oil and Analysis by FCA, Constant Volume Combustion Chamber Method (IP541)

Marine Engineering
2010English

Fabrication of High Thermal Conductivity NARloy-Z-Diamond Composite Combustion Chamber Liner for Advanced Rocket Engines

2016English

SEC Method-Based Engine Combustion Pressure Sensor

Marine Engineering
2017English

Generating Plasma by Cumulative Detonation in a Combustion Chamber

International Journal of Aerospace Engineering
Aerospace Engineering
2019English

Bankruptcy Prediction by Using the Grover Method

2019English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy