SSTO: 单段式轨道航天器 (Single-stage-to-orbit)TSTO: 双段式轨道航天器 (Two-stage-to-orbit)SSTSO: 单段式亚轨道航天器 (Si…zh.wikipedia.org|基于3个网页 3. 单段式轨道太空飞行器 SSTO: 单段式轨道太空飞行器 (Single-stage-to-orbit)TSTO: 双段式轨道太空飞行器 (Two-stage-to-orbit)SSTSO:...
1) Single stage to orbit 单级入轨火箭 2) single-stage 单级 1. Design and Experimental Studies of Single-stage and Double-stage Pulse Tube Refrigerators; 单级和两级脉冲管制冷机的设计和实验研究 2. Analysis of asingle-stagehigh power factor electronic ballast with class-E resonant inverter is ...
Over the years, several aspects of both so-called single- and two-stage-to-orbit space planes have provided many interesting research topics. Amongst others, the constrained trajectory optimisation has proven to be a challenging subject. In this chapter, an inverse-dynamics approach is combined ...
SSTOs are not exclusively required to break orbit and re-enter the atmosphere for a landing as they may be refueled in orbit. Designing a Single Stage to Orbit craft generally requires a firm grasp of spacecraft as well as aircraft design in order to create a craft that can operate both ...
Radian Aerospace is building a next-generation spaceplane planned to be the world's first single-stage-to-orbit, truly reusable space vehicle operating in Low Earth Orbit.
5) single stage to orbit 单级入轨 1. Through calculation,the veracity of the mass model was verified;optimized engine performance parameters forsingle stage to orbitwere obtained and the optimized results with. 通过计算,验证了质量模型的准确性,得到了实现单级入轨发动机的最优性能参数,给出了在当前所...
Kistler Aerospace believes the key to reusable vehicle success is to start with a small, simple, lightweight, minimum payload vehicle, that utilizes an innovative design and employs unique launch and landing systems to optimize rocketship performance, then to expand to larger configurations. This ...
SINGLE-STAGE-TO-ORBIT ROCKET 来自 掌桥科研 喜欢 0 阅读量: 9 申请(专利)号: WO2000US05126 申请日期: 2000-02-29 公开/公告号: WO0138170A1 公开/公告日期: 2001-05-31 申请(专利权)人: TECHNANOGY, LLC 发明人:LH Welch,JA Martin 摘要: A solid fueled rocket motor capable of accelerating a ...
In order to consider the possibility of a nuclear thermal rocket (NTR) ground launch, it is necessary to evaluate the risks from such a launch. This includes analysis of the radiation dose rate around the rocket, determining the rate of activation of the materials near the launch, and ...
FEASIBLILITY STUDY OF A LASER RAMJET SINGLE-STAGE-TO-ORBIT VEHICLE Momentum coupling coefficients, Cm, ofa laser ramjet vehicle are calculated by CFD and an engine cycle analysis. The flight trajectory ofthe laser ramjet v... H Katsurayama,Y Hirooka,K Komurasaki,... 被引量: 0发表: 2003年...