Fibre composite structures for space applications - Recent and future developments

Cryogenics

Volumn 38, Issue 1, 1998, Pages 51-59

  Bansemir, H ^a   Haider, O ^a  

^a EUROCOPTER DEUTSCHLAND GMBH   (France)

Author keywords

Fibre composites; Low temperature mechanical and thermal properties; Space application

Indexed keywords

EID: 0003844378     PISSN: 00112275     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0011-2275(97)00110-0     Document Type: Article

References (8)

1. Hartwig, G., Reinforced polymers at low temperatures. Presented at the ICMC/ICEC Conf., San Diego, CA, 1981.
2. Rosenberg, R., The thermal conductivity of glass-fibre and carbon-fibre/epoxy composites from 2 to 80 K. Cryogenics, 1982, May, 245.
3. Bongers, B., Haider, O. and Tauber, W., Thermal insulation of a cryogenic tank for a space telescope using a pretensioned suspension of fibre reinforced composite (FRC). UD 571-90-PUB, ECCM-4, Stuttgart, 25-28 September 1990.
4. Bansemir, H. and Haider, O., Basic material data and structural analysis of fibre composite components for space application. UD 582-90-PUB, ICMC Int. Cryogenic Materials Conf. on Nonmetallic Materials and Composites at Low Temperatures, 17-18 May 1990.
5. Ahlborn, K., Mechanische Eigenschaften und Schadensmechanismen von CFK- und GFK Verbunden bei Raumtemperatur und bei tiefen Temperaturen. Primärbericht 13*02*01P10B 09/87, Institut für Material- und Festkörperforschung IV, Kernforschungszentrum Karlsruhe.
6. Bansemir, H. and Haider, O., Strength and deformation behaviour of Kevlar and carbon composite sandwich structures for space application. In Spacecraft Structures and Mechanical Testing, ESTEC, Noordwijk, 24-26 April 1991.
7. Reed, R.P. and Goulda, M., Cryogenic properties of unidirectional composites. Cryogenics, 1994, 34(11).
8. Rapp, H., New computer codes for the structural analysis of composite helicopter structures. UD-0580-90-PUB, 17th European Rotorcraft Forum, Glasgow, UK, 18-20 September 1990.