Weight Analysis of Two-Stage-To-Orbit Reusable Launch Vehicles-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Weight Analysis of Two-Stage-To-Orbit Reusable Launch Vehicles

Published:2005-07-10 Issue: Volume: Page:
ISSN:
Container-title:41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
language:
Short-container-title:

Author:

Caldwell Richard,Franke Milton,Eklund Dean

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. Development of Hydrocarbon-Fueled Scramjet Engines: The Hypersonic Technology (HyTech) Program

2. Significance of Fuel Selection for Hypersonic Vehicle Range

3. 7Boudreau, A. H., and Liston, G. W. "Solutions for Hypersonic Airbreathing Launchers Lifting Military Payloads", AIAA 2002-5217, AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans France, September 2002.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Derivation and validation of a similarity law for free-flight wind tunnel tests of parallel stage separation;Chinese Journal of Aeronautics;2023-08

2. A Preliminary Research on a Two-Stage-To-Orbit Vehicle with Airbreathing Pre-cooled Hypersonic Engines;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02

3. A Study of Estimating Structural Weight for Reusable Launch Vehicles;Applied Mechanics and Materials;2011-07

4. TSTO Reusable Launch Vehicles Using Airbreathing Propulsion;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370

www.globalauthorid.com

TOP