Cart (Loading....) | Create Account
Close category search window
 

A method for estimating space launch vehicle parameters and technological assessment

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

3 Author(s)
Toker, K.A. ; Eng. Dev. Directorate, Roketsan Missile Ind. Inc., Ankara, Turkey ; Arkun, U. ; Tinaztepe, T.

This study is based on the work performed by the authors, in the research project funded by Turkish Ministry of Defense under the lead of the Turkish Air Force. The first aim is to develop a computer simulation model to simulate launch missions of small satellites up to medium Earth orbits. The second aim is to apply the model to a specific launch problem, evaluate the results in terms of their validity and to conclude with an assessment on the realization of the problem by the current technological infrastructure in Turkey.

Published in:

Recent Advances in Space Technologies, 2003. RAST '03. International Conference on. Proceedings of

Date of Conference:

20-22 Nov. 2003

Need Help?


IEEE Advancing Technology for Humanity About IEEE Xplore | Contact | Help | Terms of Use | Nondiscrimination Policy | Site Map | Privacy & Opting Out of Cookies

A not-for-profit organization, IEEE is the world's largest professional association for the advancement of technology.
© Copyright 2014 IEEE - All rights reserved. Use of this web site signifies your agreement to the terms and conditions.