Amanote Research

Amanote Research

    RegisterSign In

Starsaber - A Small Payload-Class TSTO Vehicle Concept Utilizing Rocket-Based Combined Cycle Propulsion

doi 10.2514/6.2001-3516
Full Text
Open PDF
Abstract

Available in full text

Date

July 8, 2001

Authors
Brad StJohn OldsLaura LedsingerJames McIntireDouglas NelsonJohn Weglian
Publisher

American Institute of Aeronautics and Astronautics


Related search

Rocket Propulsion Powered Using a Gyrotron

Journal of Energy and Power Engineering
2017English

Supersonic Multi-Objective Optimization of a Rocket Based Combined Cycle Inlet by Differential Evolution

English

Ducted Rocket Propulsion Technology.

Journal of the Japan Society for Aeronautical and Space Sciences
1991English

Rocket Propulsion : Classification of Different Types of Rocket Propulsion System and Propulsive Efficiency

International Journal of Engineering Applied Sciences and Technology
2019English

Rocket Propulsion Thirty Years Ago

Nature
Multidisciplinary
1961English

Simulation of a Rocket Base Combined Cycle Exchange Inlet at Subsonic Conditions

English

Characterization of Nal Powders for Rocket Propulsion

2011English

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

1997English

Antimatter Induced Fission for Nuclear Rocket Propulsion

2006English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy