Hybrid rocket engines are flexible, safe, reliable, and low-cost and can be used in many aerospace applications. The engine design and operation are contingent on the type of designated mission and engine design is strictly related to trajectory optimization. In real-world applications, ...
Hybrid Rocket Engine exists since the dawn of aerospace industry. The problem is: it does not scale. And that’s where we came in: we find a way to make it scalable. Basically, what we did is start hybrid rocket engine design from scratch and ended it up completely modifying the whole...
Shimada, "Conceptual design of single-stage launch vehicle with hybrid rocket engine for Scientific observation using design informatics", Journal of Space Engineering, vol. 6, no. 1, pp. 15-27, 2013.K. Chiba, M. Kanazaki, M. Nakamiya, K. Kitagawa, and T. Shimada, "Conceptual design ...
is no exception. Believe it or not, this latest wild automotive concept is visually less extreme than his others. Fluid yet sharp, the design sees a single driver in a cockpit centered around a “living and breathing” shell with an advanced self-healing skin that automatically repairs small ...
A single-stage launch vehicle with hybrid rocket engine has been conceptually designed by using design informatics, which has three points of view, i.e., problem definition, optimization, and data mining. The primary objective of the present design is that the down range and the duration time ...
The Japanese domestic production of commercial grade (C/G) hydrogen peroxide (HP) for chemical industries are more than 300,000 tons/year (reduced 100%) but its concentration has been currently regulated below 60% for handing, storages and shipping safety, no 90% rocket grade (R/G) HP has...
美 英 un.混合式火箭发动机 例句
2. Design premises This publication presents the process of mathematical modelling of the hybrid rocket engine operating parameters (in the context of creating a preliminary design of a rocket engine). During the development of the discussed model, a thorough analysis has been performed in an effort...
In the present study a multi-objective design optimization of a rocket based combined engine has been performed. Objective functions are specific impulse a... D Pastrone,MR Sentinella - 《Journal of Propulsion & Power》 被引量: 0发表: 2009年 Papers : Preliminary Design of Hybrid Rocket Based...
Hybrid rocket propulsion can contribute to reduce launch costs by simplifying engine design and operation. Hypergolic propellants, i.e. igniting spontaneously and immediately upon contact between fuel and oxidizer, further simplify system integration by removing the need for an ignition system. Such ...