RITD Project Conference Contributions

Overview of the Conference Contributions

The following conference contributions resulted from the RITD project. Some of the conference presentations will took place after the official end of the project, but they are included also here.

  1. J. Heilimo, et. al., Adapting Mars Entry, Descent and Landing System for Earth, Vol. 7 EPSC2012-296 2012, European Planetary Science Congress 2012, Madrid, Spain, 23.-28. September 2012.
  2. J. Heilimo, et. al., Adapting Mars Entry, Descent and Landing System for Earth, IPPW-9 Session 6B Earth Entry and Sample Return, Toulouse, France, 18.-22. June 2012.
  3. J. Heilimo, et. al., Adapting Mars Entry, Descent and Landing System for Earth, Vol. 8, EPSC2013-515 2013, European Planetary Science Congress 2013, London, UK, 8.-13. September 2013.
  4. V. V. Koryanov, Research of the Dynamics Motion of Landing Vehicle with Inflatable Braking Device in the Planet Atmosphere, Paper ID: 17433, oral, 64th International Astronautical Congress 2014, Beijing, China, 24.-27. September 2013.
  6. J. Heilimo, et. al., RITD - Re-entry: Inflatable Technology Development in Russian Collaboration
  7. V. V. Koryanov, et. al., Study of the Dynamic of Motion Landing Vehicles in the Planets Atmosphere Using Inflatable Braking Device, B0.2-0045-14-oral, 40th COSPAR Scientific Assembly 2014, Moscow, Russia, 2.-10. August 2014.
  8. V. V. Koryanov, et. al., Method of Calculating the Descent of the Spacecraft in the Atmosphere Using Technology Adaptation Landing in Different Environmental Conditions, Paper ID: 23247, oral,
  9. J. Heilimo, et. al., RITD - Re-entry: Inflatable Technology Development in Russian Collaboration, Vol. 9, EPSC2014-232, 2014, European Planetary Science Congress 2014, Cascais, Portugal, 7.-12. September 2014.
  12. H. Haukka, et. al., , Vol. 17, EGU2015-15356-1, 2015, EGU General Assembly 2015, Austria, Vienna, 12.-17. April 2015.
  13. J. Heilimo, et. al., Adapting Mars Entry, Descent and Landing System for Earth, Vol. 17, EGU2015-15365-1, 2015, EGU General Assembly 2015, Austria, Vienna, 12.-17. April 2015.
  14. H. Haukka, et. al., RITD - Adapting Mars Entry, Descent and Landing System for Earth, Vol. 10, EPSC2015-567, 2015 European Planetary Science Congress 2015
  15. V. V. Koryanov, et. al., Analysis of the dynamics of movement of the landing vehicle with an inflatable braking device on the final trajectory under the influence of wind load, Vol. 10, EPSC2015-464, 2015 European Planetary Science Congress 2015

Overview of the RITD related Articles

  1. V.P. Kazakovtsev, V.V. Koryanov, "The method of studying the dynamics of angular motion space landing vehicle with ballute device", Bulletin of Bauman Moscow State Technical University, 2012.
  3. V.V. Koryanov, V.P. Kazakovtsev,
  4. V.V. Koryanov, V.P. Kazakovtsev,