A User's Primer for Comparative Assessments of All-Rocket and Rocket-Based Combined-Cycle Propulsion Systems for Advanced Earth-to-Orbit Space Transport Applications

机译：用于入门级太空火箭应用的全火箭和火箭联合循环推进系统比较评估的用户入门手册

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The contex here is quick-look assessments of advanced space transportation systems for Earth-to-orbit operations for the full range of propulsion approaches. In the format of a "user's primer" this paper offers a simple, readily accessible graphical approach, for making fast, accurate, back-of-the-envelope level combparisons between vehicle systems powered by both all-rocket and airbreating/rocket propulsion combinations. It is based on the ideal rocket equation and a wider-utility variant of it, which is here introduced with fully-derived mathematical coverage (Appendix 1).

机译：这里的Contex是对全系列推进方法的地球对轨道操作的先进空间运输系统的快速看法。在“用户底漆”的格式中，本文提供了一种简单，易于访问的图形方法，用于制作快速，准确，背包的后置级别的车辆系统之间，由全火箭和空气堆叠/火箭推进组合提供动力。它基于理想的火箭方程和它的更广泛的实用性变体，这里以完全导出的数学覆盖率引入（附录1）。

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《31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 10-12, 1995/San Diego, CA》||p.1-22|共22页
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William J.D.Escher; Eric H.Hyde; David M.Anderson;
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中图分类航空;
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1. EARTH-TO-ORBIT SPACE TRANSPORTATION SYSTEM [J] . A. A. Sergienko, Weizing Zhou Russian Aeronautics . 2005,第2期

机译：地球到轨道空间运输系统
2. Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems [J] . A. V. Bogatyi, R. V. El’nikov, I. P. Nazarenko, Russian Aeronautics . 2018,第3期

机译：作为小型航天器推进系统的一部分，先进的脉冲等离子体推进器及其应用
3. A generalization of the rocket formula and its application to advanced space propulsion systems [J] . L.Nasi, J.-L.Raimbault Acta astronautica . 2011,第1a2期

机译：火箭公式的推广及其在先进空间推进系统中的应用
4. A U.S. history of airbreathing/rocket combined-cycle (RBCC) propulsion for powering future aerospace transports, with a look ahead to the year 2020 [C] . Escher William J. D. International Symposium on Air Breathing Engines . 1999

机译：AS.避风气/火箭综合循环（RBCC）推进的历史，用于推动未来航空航天运输，并展望2020年
5. Investigation of a Cluster of High-power Helicon Thrusters for Advanced In-space Electric Propulsion Applications [D] . Vereen, Keon L. 2019

机译：用于高功率直升机推进器的高功率直升机推动簇调查
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8. Supersonic Wind Tunnel Tests of a Half-Axisymmetric 12 deg-Spike Inlet to a Rocket-Based Combined-Cycle Propulsion System [R] . DeBonis, J. R. , Trefny, C. J. 2001

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A User's Primer for Comparative Assessments of All-Rocket and Rocket-Based Combined-Cycle Propulsion Systems for Advanced Earth-to-Orbit Space Transport Applications

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