Damage Tolerance Of Candidate Thermoset Composites For Use On Single Stage To Orbit Vehicles
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Author | : A. T. Nettles |
Publisher | : |
Total Pages | : 56 |
Release | : 1994 |
Genre | : Composite materials |
ISBN | : |
Abstract: Four fiber/resin systems were compared for resistance to damage and damage tolerance. One toughened epoxy and three toughened bismaleimide (BMI) resins were used, all with IM7 carbon fiber reinforcement. A statistical design of experiments technique was used to evaluate the effects of impact energy, specimen thickness, and tup diameter on the damage area as computed by C-scans, and residual compression-after-impact (CAI) strength. Results showed that two of the BMI systems sustained relatively large damage zones yet had an excellent retention of CAI strength.
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Total Pages | : 994 |
Release | : 1995 |
Genre | : Aeronautics |
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Total Pages | : 1484 |
Release | : 1995 |
Genre | : Government publications |
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Total Pages | : 1482 |
Release | : 1995 |
Genre | : Government publications |
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Total Pages | : 624 |
Release | : 1995 |
Genre | : Science |
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Total Pages | : 180 |
Release | : 1997 |
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Total Pages | : 92 |
Release | : 1994 |
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Total Pages | : 472 |
Release | : 1994 |
Genre | : Aeronautics |
ISBN | : |
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 52 |
Release | : 2018-07-08 |
Genre | : |
ISBN | : 9781722332457 |
Four fiber/resin systems were compared for resistance to damage and damage tolerance. One toughened epoxy and three toughened bismaleimide (BMI) resins were used, all with IM7 carbon fiber reinforcement. A statistical design of experiments technique was used to evaluate the effects of impact energy, specimen thickness, and impactor diameter on the damage area, as computed by C-scans, and residual compression-after-impact (CAI) strength. Results showed that two of the BMI systems sustained relatively large damage zones yet had an excellent retention of CAI strength. Nettles, A. T. and Lance, D. and Hodge, A. Marshall Space Flight Center...
Author | : |
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Total Pages | : 692 |
Release | : 1995 |
Genre | : Ceramic materials |
ISBN | : |