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Aerospace Materials: TI-5AL-2.5SN SHEET UNK

Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).

Materials Sciencematerial id: TI-5AL-2.5SN SHEET UNK9 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Fbru ksi (ksi)Fbru ksi 2 (ksi)Fbry ksi (ksi)Fbry ksi 2 (ksi)Fcy ksi (ksi)Fcy ksi LT (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Fty ksi (ksi)Fty ksi LT (ksi)basisdensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)form
TI-5AL-2.5SN SHEET UNK ANY A T5 3 1 0b C27015.515.516725013319011511875120120110113A0.1621010Sheet, strip, and plate
TI-5AL-2.5SN SHEET UNK ANY A T5 3 1 0b C47015.515.516725013319011811875120120113113A0.1621010Sheet, strip, and plate
TI-5AL-2.5SN SHEET UNK ANY A T5 3 1 0b C67015.515.516725013319011811875120120113113A0.1621010Sheet, strip, and plate
TI-5AL-2.5SN SHEET UNK ANY B T5 3 1 0b C37015.515.517926813919812012380128129115118B0.162Sheet, strip, and plate
TI-5AL-2.5SN SHEET UNK ANY B T5 3 1 0b C57015.515.518327514220312312682131132118121B0.162Sheet, strip, and plate
TI-5AL-2.5SN SHEET UNK ANY B T5 3 1 0b C77015.515.519028514721012813085135137123125B0.162Sheet, strip, and plate
TI-5AL-2.5SN SHEET UNK ANY S T5 3 1 0b C17015.515.516725013319011511875120120113113S0.1621010Sheet, strip, and plate
TI-5AL-2.5SN SHEET UNK ANY S T5 3 1 0b C87015.515.516725013319011811875120120113113S0.1621010Sheet, strip, and plate
TI-5AL-2.5SN SHEET UNK ANY S T5 3 1 0b C97015.515.5115115110110S0.1621010Sheet, strip, and plate

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