System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
doi 10.2322/tastj.12.pa_91
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Japan Society for Aeronautical and Space Sciences

Related search

Application of a New Economic Analysis Tool to a Two-Stage-To-Orbit RBCC Launch Vehicle Design

1996English

Evaluation of Multidisciplinary Optimization Techniques Applied to a Reusable Launch Vehicle

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
2006English

Performance of a RBCC Engine in Rocket-Operation

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
2012English

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

1997English

Hydrocarbon Pollutant Emitted From a Diesel Engine Fueled With Biodiesel and Diesel Fuel No.2

Energy Review
2014English

Multi-Disciplinary System Design Optimization of a Launch Vehicle Upper-Stage

Journal of Aerospace Technology and Management
Aerospace Engineering
2017English

Concept Study of a Reusable Suborbital Launch Vehicle

2018English

Cargo Transfer and Return Vehicle and Personnel Launch System Launch Processing Model

English

How Small Can a Launch Vehicle Be?

2005English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy