✦ LIBER ✦

Optimal design for hybrid rocket engine for air launch vehicle

✍ Scribed by Ihnseok Rhee; Changjin Lee; Jae-Woo Lee

Book ID: 107624416
Publisher: Springer-Verlag
Year: 2008
Tongue: English
Weight: 605 KB
Volume: 22
Category: Article
ISSN: 1738-494X
DOI: 10.1007/s12206-008-0514-6

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Cost Engineering – The new paradigm for

Cost Engineering – The new paradigm for space launch vehicle design

✍ Dietrich E. Koelle 📂 Article 📅 1998 🏛 Springer ⚖ 430 KB

Design and optimization of variable thru

Design and optimization of variable thrust hybrid rocket motors for sounding rockets

✍ DaLin Rao; GuoBiao Cai; Hao Zhu; Hui Tian 📂 Article 📅 2011 🏛 SP Science China Press 🌐 English ⚖ 939 KB

Determination of optimal trajectory unde

Determination of optimal trajectory under design constraints for a satellite launch vehicle

✍ Shashi Kant Shrivastava; M.Narayan Reddy 📂 Article 📅 1976 🏛 Elsevier Science 🌐 English ⚖ 569 KB

Two hybrid differential evolution algori

Two hybrid differential evolution algorithms for engineering design optimization

✍ T. Warren Liao 📂 Article 📅 2010 🏛 Elsevier Science 🌐 English ⚖ 631 KB

The computing of the optimal power consu

The computing of the optimal power consumption for semi-track air-cushion vehicle using hybrid generalized extremal optimization

✍ Dong Xie; Zhe Luo; Fan Yu 📂 Article 📅 2009 🏛 Elsevier Science 🌐 English ⚖ 354 KB

Design optimization of switched reluctan

Design optimization of switched reluctance machines for starter/generator of hybrid electric vehicle by genetic algorithm

✍ Jawad Faiz; K. Moayed-zadeh 📂 Article 📅 2009 🏛 John Wiley and Sons 🌐 English ⚖ 188 KB

## Abstract A switched reluctance machine for starter/generator of a hybrid electric vehicle is designed to optimize two objective functions: (1) high starting torque over low speed and (2) high efficiency over high speed. For static modeling of flux‐linkage, a quick analytical model is used and it