Multi-frequency dynamic absorber for improved spacecraft comfort during the launch phase [0.03%]
用于提升航天器发射阶段舒适度的多频动态吸振器
Mastroddi, Franco; Facchini, Gianluca; Gaudenzi et al.
Mastroddi et al.
Life prediction of thermally highly loaded components: modelling the damage process of a rocket combustion chamber hot wall [0.03%]
热负荷高部件的寿命预测：火箭燃烧室热壁损伤过程的建模
W. Schwarz; S. Schwub; K. Quering; D. Wiedmann; H. W. Höppel; M. Göken
W. Schwarz; S. Schwub; K. Quering; D. Wiedmann; H. W. Höppel; M. Göken
Weak stability boundary transfer to the Moon from GTO as a piggyback payload on Ariane 5 [0.03%]
作为“阿丽亚娜5”火箭的搭载体，从地球同步转移轨道向月球进行弱稳定性边界转移
Quantius, Dominik; Spurmann, Jörn; Dekens et al.
Quantius et al.
L. Scialino,A. Ihle,M. Migliorelli et al.
L. Scialino et al.
V. Fraux,M. Lawton,J. R. Reveles et al.
V. Fraux et al.
Study of a very large reflectarray antenna built with unfoldable panels for missions from L to C band [0.03%]
Renaud Chiniard,Ludovic Schreider,Nicolas Girault et al.
Renaud Chiniard et al.
Leri Datashvili
Leri Datashvili
Large deployable antennas [0.03%]
T. K. Henriksen,C. Mangenot
T. K. Henriksen
Investigation of the turbulent wake flow of generic launcher configurations via a zonal RANS/LES method [0.03%]
Statnikov, V.; Meiß, J.-H.; Meinke et al.
Statnikov et al.
Santiago-Prowald, J.; Baier, H.
Santiago-Prowald