Body Material |
N/A Butyl |
Wire Material |
N/A Steel |
Flange Material |
N/A Plate Steel |
Cable Material |
N/A Galvanized Steel Aircraft Cable |
Root Ring Material |
N/A Steel |
Bolt Hole |
N/A Threaded |
Size I.D. |
N/A 10 in |
F/F |
N/A 8 in |
Vacuum |
N/A 16 inHg |
Maximum Pressure PSI at 170 deg F |
N/A 225 psi |
Axial Compression |
N/A 0.75 in |
Compression Force |
N/A 398 lbs |
Axial Elongation |
N/A 0.25 in |
Elongation Force |
N/A 455 lbs |
Lateral Deflection |
N/A 3/4 in |
Lateral Force |
N/A 781 lbs |
Angular |
N/A 15 ยบ |
Deflection_Weight |
N/A 68 lbs |
No. of Cables |
N/A 4 |
No. Bolt Holes |
N/A 12 |
Hole Size |
N/A 7/8-9NC |
Cable Distance |
N/A 14.25 in |
Cable Diameter |
N/A 0.35 in |
SPRING RATE |
N/A TBD lb/in |
Flow Coefficient |
N/A TBD |
Weight |
N/A 68 lb |
