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Almar 20

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Journal Articles
Alloy Digest (1964) 13 (4): SA-162.
Published: 01 April 1964
... ALMAR 20 is a high nickel martensitic steel which is strengthened by precipitation hardening. It has excellent combination of strength and toughness particularly in the presence of notches and cracks. It is recommended for applications such as solid fuel rocket cases and aircraft landing gear...
Journal Articles
Alloy Digest (1970) 19 (2): SS-234.
Published: 01 February 1970
... ALLEGHENY ALMAR-362 is an age-hardenable martensitic stainless steel recommended for applications requiring high strength and good corrosion resistance, such as aircraft and missile structures, hydraulic and pneumatic equipment components, and in the chemical processing industry. This datasheet...
Journal Articles
Alloy Digest (1967) 16 (4): SA-208.
Published: 01 April 1967
... ALMAR 362 is a maraging stainless steel having high corrosion and oxidation resistance. It has good workability and weldability with low rate of work hardening. It is recommended for chemical processing and industrial equipment industries requiring high strength material with outstanding corrosion...
Journal Articles
Alloy Digest (1963) 12 (9): SA-154.
Published: 01 September 1963
... Almar 25 (1.37 percent titanium, .076 inch thick). I - , - I- l- 120 210 loo I 40 30 s d : 20 a % 10 290 280 270 i D. 260 -d . f Is0 : : I P 140 c s n 130 900 -1ooOF and marwmpercd at indicated rempcmrures.) Tensile Yield RedUCriO Srrcngrh SCIC ph EIO gadO of Area p psi si (0.2%) Sin ? % 265000...
Journal Articles
Alloy Digest (1978) 27 (7): SA-349.
Published: 01 July 1978
... ALMAR 300 Alloy is a vacuum-melted ultra-high-strength steel. The annealed structure of this alloy is essentially a carbon-free, iron-nickel martensite (a relatively soft Rockwell C 28) that can be strengthened by cold working and elevated-temperature (900-950 F) age hardening to useful yield...
Journal Articles
Alloy Digest (1963) 12 (10): SA-156.
Published: 01 October 1963
... ALMAR 18 is a high-nickel martensitic steel which is strengthened by precipitation hardening. It has excellent combination of strength and toughness particularly in the presence of notches or cracks. It is recommended for applications such as solid fuel rocket cases and aircraft landing gears. It...
Journal Articles
Alloy Digest (1974) 23 (7): SS-297.
Published: 01 July 1974
... FATIGUE Test Charpy Impact* Temperature (V-Notch) ft-lb Rockwell Fatigue Strengtht C ( 106 cycw oF Longitudinal Transverse Hardness psi 70 185 135 28 66000tt 20 170 I35 - 0 130 SO - -50 30 I2 -100 6 6 *Specimens made from annealed K-in. plate. TTension-tension fatigue tests (Min. stress to max. stress...