Print Email Facebook Twitter Spacecraft sustained load fracture control Title Spacecraft sustained load fracture control Author Wanhill, R.J.H. Institution National Aerospace Laboratory NLR Date 1989-05-10 Abstract The opportunities for sustained load fracture control in spacecraft are indicated. Emphasis is given to verification by small-scale laboratory testing. Subject stress corrosion crackinghydrogen embrittlementfracture mechanicsaluminium alloystitanium alloyshigh strength steelsnickel alloyshigh strength alloyshydraulic fluidsfatigue testsspacecraft environmentsspace shuttle orbitersfatigue life To reference this document use: http://resolver.tudelft.nl/uuid:00506e01-c041-49b5-80f7-2109fec7a8e5 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR Technical Publication TP 89163 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1989 National Aerospace Laboratory NLR Files campus only