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

doi 10.2514/6.1996-4092
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

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
2014English

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

Journal of Aerospace Technology and Management
Aerospace Engineering
2017English

Ascent Trajectory Optimisation for a Single-Stage-To-Orbit Vehicle With Hybrid Propulsion

2012English

Application of an Automated Aircraft Architecture Generation and Analysis Tool to Unmanned Aerial Vehicle Subsystem Design

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Mechanical EngineeringAerospace Engineering
2014English

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

1997English

Application of Air Diffuser for Thermostating of a Launch Vehicle

Scientific notes of Taurida National V.I. Vernadsky University. Series: Technical Sciences
2019English

Evaluation of Multidisciplinary Optimization Techniques Applied to a Reusable Launch Vehicle

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
2006English

Design and Analysis of a Two Stage Reduction Gearbox

International Journal of Mechanical and Production Engineering Research and Development
Transfer ProcessesFluid FlowMechanical EngineeringAerospace Engineering
2018English

The Design of a Kerosene Turbopump for a South African Commercial Launch Vehicle

2012English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy