Amanote Research

Amanote Research

  • Register
  • Sign In

Integrated Design Methodology for Highly Reliable Liquid Rocket Engine

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

doi 10.2322/jjsass.54.403

Full Text

Abstract

Available in

Date

January 1, 2006

Authors

Naoshi KurataniHiroshi AokiMasaaki YasuiHirotaka KureGoro Masuya

Publisher

Japan Society for Aeronautical and Space Sciences


Related search

SCORES-2 Design Tool for Liquid Rocket Engine Analysis

2002French

Radial Turbine Preliminary Aerodynamic Design Optimization for Expander Cycle Liquid Rocket Engine

2006English

Design of a Highly Integrated and Reliable SDR Platform for Multiple RF Applications on Spacecrafts

2017English

An Integrated Design Methodology

Proceedings of the Canadian Engineering Education Association (CEEA)
2011English

Integrated Two-Cylinder Liquid Piston Stirling Engine

Applied Physics Letters
AstronomyPhysics
2014English

SCCREAM (Simulated Combined-Cycle Rocket Engine Analysis Module) - A Conceptual RBCC Engine Design Tool

1997French

Dynamic Behavior of Control Valves of a Liquid Rocket Engine Feeding System

The International Conference on Applied Mechanics and Mechanical Engineering
2006English

A SPINEware Based Computational Design Engine for Integrated Multi-Disciplinary Aircraft Design

2002English

An Integrated Modeling Methodology for Material Handling Systems Design

English

Amanote Research

Note-taking for researchers

Follow Amanote


© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy