A porous flow control element for pulsed plasma thrusters Hannah BöhrkMatthias LauHans-Peter Röser Original Paper 08 October 2011 Pages: 1 - 6
Depressurization solutions of vented enclosures during launch Ronald C. DykhuizenWalter GillLarry A. Bruskas Original Paper 26 November 2011 Pages: 7 - 12
Methodologies for launcher–payload coupled dynamic analysis S. H. J. A. Fransen Original Paper 23 August 2011 Pages: 13 - 25
European Space Agency’s launcher multibody dynamics simulator used for system and subsystem level analyses Gianluigi BaldesiMario Toso Original Paper 24 January 2012 Pages: 27 - 48
Weak stability boundary transfer to the Moon from GTO as a piggyback payload on Ariane 5 Dominik QuantiusJörn SpurmannHartmut Päsler Original Paper 21 April 2012 Pages: 49 - 59
Investigations on the thermal behaviour of CMC-based leading edges in hypersonic arc jet flows Markus KuhnBurkard EsserLuca Cavagna Original Paper 27 April 2012 Pages: 61 - 76