1 |
Bellini, M. and Calvi, A. (2014), "Dynamic analysis and loads definition for the structural design of the Euclid spacecraft", ISMA 2014-USD 2014 Conference, Leuven, Belgium, September.
|
2 |
ESA Mechanical shock design and verification handbook (2012), ESSB-HB-E-005, Noordwijk, The Netherlands, April.
|
3 |
Racca, G.D. et al. (2014), The Euclid Spacecraft Design, IAC-14-A7.1.3., 65th Int. Astronautical Congress (IAC 2014), Toronto, Canada.
|
4 |
Salvignol, J.C., Laine, B., Ngan, I., Honnen, K. and Kommer, A. (2009), "Notching during random vibration test based on interface forces", The JWST NIRSpec Experience, 11th ECSSMMT, European Conference on Spacecraft Structures, Materials & Mechanical Testing, Toulouse, France, September.
|
5 |
Scharton, T.D. (1997), Force Limited Vibration Testing Monograph, NASA Reference Publication RP-1403, May.
|
6 |
Soyuz User's Manual (2012), Issue 2 Rev. 0, March.
|
7 |
Spacecraft Mechanical Loads Analysis Handbook (2013), ECSS-E-HB-32-26A, Noordwijk, The Netherlands, February.
|
8 |
Structural factors of safety for spaceflight hardware (2009), ECSS-E-ST-32-10C Rev. 1, Noordwijk, The Netherlands, March.
|