The tensile, compressive, fatigue, thermal expansion, thermal conducti
vity and specific heat of unidirectional laminates reinforced with bor
on, alumina, aramid, S-glass, E-glass, and high strength, high modulus
and medium modulus carbon fibres are reviewed. The ratio of strength
to thermal conductivity is used to assess the suitability of various f
ibre-reinforced laminates for supporting struts (experiencing compress
ion) or straps (experiencing tension) at cryogenic temperatures. The r
elationships between laminate properties and reinforcement fibres are
discussed.