Close category search window
 

Balloon precursor mission for Venus Surface Sample Return

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)
Kerzhanovich, V.V. ; Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA ; Hall, J. ; Yavrouian, A.

This paper proposes a precursor mission to the Venus Surface Sample return Mission (VSSR). The present scenario of the VSSR includes delivery by a balloon of the Venus Ascent Vehicle (VAV) from the surface to an altitude of approximately 60 km, where it can be launched without huge penalty for atmospheric losses. The mission includes a number of critical technologies that can be validated in this proposed precursor mission. The other objective of the proposed mission is to collect more accurate data on the Venus atmosphere that is essential for the VSSR mission design. The paper discusses the basic mission and system elements for the proposed precursor mission

Published in:
Aerospace Conference, 2001, IEEE Proceedings.  (Volume:1 )

Date of Conference: 2001

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 2013 IEEE - All rights reserved. Use of this web site signifies your agreement to the terms and conditions.