L
ong
D
uration
E
xposure
F
acility
(LDEF) Archive System
NASA Langley Research Center
Hampton, Virginia
Impact Damage of LDEF Surfaces
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Responsible Parties:
Page Content:
William H. Kinard
Page Construction:
Thomas H. See
Click on Thumbnail or Title for larger view.
PAO Picture
897.66 Kb
784 x 981
S32-85-009
621.68 Kb
760 x 761
S32-85-029
632.31 Kb
760 x 759
S32-85-062
459.78 Kb
584 x 804
S32-85-39
548.46 Kb
760 x 764
Classic Impact
into Aluminum
277.21 Kb
441 x 388
Doublet Impact
into Aluminum
246.06 Kb
441 x 388
Aluminum Impact
237.84 Kb
644 x 486
Aluminum Penetration
280.15 Kb
515 x 472
Painted Aluminum
120.97 Kb
512 x 512
Beta Cloth
196.93 Kb
904 x 752
Beta Cloth 2
156.94 Kb
904 x 1010
Largest LDEF
Impact (5.25 mm)
Teflon-coated Aluminum
321.40 Kb
581 x 592
Largest LDEF Impact
Side View
110.57 Kb
407 x 332
Blanket Penetration
436.45 Kb
549 x 700
Blanket Penetration 2
242.54 Kb
441 x 496
Crater/Ejecta
Deposit
56.78 Kb
589 x 531
Ejecta on
Aluminum
391.48 Kb
589 x 562
Ejecta on
Germanium
78.50 Kb
776 x 602
Germanium
252.79 Kb
510 x 494
LDEF Grapple
Fixture
34.01 Kb
454 x 399
Aluminum Crater
263.88 Kb
512 x 512
Low-Velocity
Impact in Aluminum
264.67 Kb
441 x 496
Metal-Silica
-Oxide (MOS) Detector
430.22 Kb
592 x 695
On-Orbit A0178
Teflon Thermal Blanket
79.63 Kb
666 x 555
On-Orbit A0178
Teflon Thermal Blanket
53.60 Kb
640 x 480
On-Orbit A0178
Teflon Thermal Blanket
37.86 Kb
395 x 347
On-Orbit A0178
Teflon Thermal Blanket
96.39 Kb
790 x 694
Painted Aluminum
Spall & Shock Effects
205.76 Kb
512 x 592
Painted Aluminum
Oblique View
104.18 Kb
857 x 526
Painted Aluminum
Oblique View 2
53.22 Kb
759 x 547
Painted Aluminum
Penetration
247.55 Kb
544 x 525
Painted Aluminum
Spall Area
202.23 Kb
589 x 531
Painted Aluminum
Spall Area 2
366.36 Kb
705 x 740
Painted Aluminum
Spall Area 3
53.50 Kb
310 x 280
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