Mechanical Qualification Test Campaign on the Demise Observation Capsule
Commenced in January 2007
Frequency: Monthly
Edition: International
Paper Count: 33035
Mechanical Qualification Test Campaign on the Demise Observation Capsule

Authors: B. Tiseo, V. Quaranta, G. Bruno, R. Gardi, T. Watts, S. Dussy

Abstract:

This paper describes the qualification test campaign performed on the Demise Observation Capsule DOC-EQM as part of the Future Launch Preparatory Program FLPP3. The mechanical environment experienced during launch ascent and separation phase was first identified and then replicated in terms of sine, random and shock vibration. The loads identification is derived by selecting the worst possible case. Vibration and shock qualification test performed at CIRA Space Qualification laboratory is herein described. Mechanical fixtures’ design and validation, carried out by means of FEM, is also addressed due to its fundamental role in the vibrational test campaign. The Demise Observation Capsule (DOC) successfully passed the qualification test campaign. Functional test and resonance search have not been point any fault and damages of the capsule.

Keywords: Capsule, demise, DOC, launch environment, Re-Entry, qualification.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.3455597

Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 571

References:


[1] S(&)T: Demise Observation Capsule (DOC) for re-entry science and safety, http://stcorp.nl/highlights/demise-observation-capsule-doc-re-entry-science-and-safety/Junaury 2019.
[2] R. Gardi, G. Pezzella, S. Franchitti, R. Borrelli, C. Pirozzi, V.Quaranta, B. Tiseo, G. Bruno, “Additive Layer Manufacturing For Entry Capsules”, 68th International Astronautical Congress (IAC), Adelaide, Australia, 2017.
[3] M. J. Kristensen, L.Ghizoni, P. Koch, DOC-PL-GS-0004 FLPP3,” Demise Observation Capsule (DOC) D24 Avionics and instrumentation Test Plan” , Issue1.4, February 2016.
[4] NASA, “Preferred Reliability Practices, practice no. pd-ed-1259, Acoustic Noise Requirement” ,May 1996.
[5] A. Calvi “Spacecraft Loads Analysis-An Overview, http://www.ltas-vis.ulg.ac.be/cmsms/uploads/File/CALVI_Students_LIEGE_2011_6.pdf,Junuary 2019.
[6] DOC S&T team,”DOC-PL-ST-0003-v1.5 D29 EQM-PFM Test Verification and Validation Plan”,2017
[7] Arianespace, Ariane 5 User’s Manual, Issue 5 Revision 2 ,2016 Roland Lagier, page 3-11.
[8] Arianespace, Vega User’s Manual, 2014
[9] Arianespace , Soyuz User’s Manual, 2012
[10] Arianspace Direction Commerciale Technical Support Department, Ariane Structure for Auxiliary Payload 5 –User’s Manual, Issue 1 – Revision 0 – May 2000.