Improving of technical characteristics of launch vehicles with liquid rocket engines using active onboard de-orbiting systems

Author:

Trushlyakov V.,Shatrov Ya.

Funder

Ministry of Education and Science

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference22 articles.

1. Update of the IADC Space Debris Mitigation Guidelines. IADC-11-02. Beijing.

2. Secretariat report. Measures taken by space agencies for reducing the growth of space debris and its potential danger. Committee on the Peaceful Uses of Outer Space for Peaceful Purposes, 13.12.1996. [Electronic resource]. – URL: http://www.unoosa.org/pdf/reports/ac105/AC105_663R.pdf. – (Accessed on: 22 January 2016).

3. The Research of the Ways of Reducing Rocket Separated Parts Impact Areas;Kompaniets,1990

4. Bases of LV Design. Choosing the Main Design Characteristics and Forming the Structural Design;Kurenkov,2011

5. R.P. Patera et al. Controlled deorbit of the «Delta-4» upper stage for the DMSP-17 mission, in: Proceedings of the 2nd IAASS Conference «Space Safety in a Global World», 14-16 May, 2007, Chicago, USA (ESA SP-645, July 2007.

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