Static performance modeling and simulation of the staged combustion cycle LPREs
- 10 January 2019
- journal article
- research article
- Published by Elsevier BV in Aerospace Science and Technology
- Vol. 86, 30-46
- https://doi.org/10.1016/j.ast.2018.12.035
Abstract
No abstract availableKeywords
This publication has 20 references indexed in Scilit:
- Multi-objective multidisciplinary design of Space Launch System using Holistic Concurrent DesignAerospace Science and Technology, 2014
- An approach for space launch vehicle conceptual design and multi-attribute evaluationAerospace Science and Technology, 2013
- Characterization of the startup and pressure blowdown processes in rocket nozzlesAerospace Science and Technology, 2013
- A Method for Simulation of a Cryogenic Liquid Propellant EngineApplied Mechanics and Materials, 2011
- Steady State Library for Liquid Rocket Engine Cycle DesignPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2011
- A study on versatile simulation of liquid propellant rocket engine systems transientsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- A modular method for the analysis of liquid rocket engine cyclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Modeling space shuttle main engine using feed-forward neural networksJournal of Guidance, Control, and Dynamics, 1994
- Digital Computer Analysis of Transients in Liquid Rocket EnginesJournal of Jet Propulsion, 1958
- Dynamics of a Variable Thrust, Pump Fed, Bipropellant, Liquid Rocket Engine SystemJournal of Jet Propulsion, 1957