Ben,
From Comsteel info for Hy-Tuf:
Related Specifications AMS6418
0.25% C, 1.30% Mn, 1.80% Ni, 0.35% Cr, 0.40% Mo, 1.50% Si
Tensile strength 1500 - 1650 MPa
From MMPDS-01, which replaced Mil handbook 5
Hi-Tuf, specification AMS6425 (not AMS6481!!)
Tensile strength 220 ksi (1517 MPa)
This is similar to what Comsteel say, but I still have the belief that when I looked in the old mil hdbk 5, they a considerably lower tensile strength for AMS6481. I dont have a copy of this handbook now to check (I guess I could download it).
The more I think about this, I may not have converted from ksi to MPa, but just compared the tensile strength to that for 4340 in an adjacent column (260 ksi), but reading the notes, values for 4340 are applicable to "consumable-electrode vacuum-melted material only".
The other curious thing is that MMPDS-01 does not appear to have anything on AMS6481, whereas I was sure it was in mil hdbk 5.
BTW:
MMPDS-01 is the only source for for material strength properties and design values that the US FAA generally accepts for complience with Federal Aviation Regulations.
AMS is the abreviation for Aerospace Material Specification
MMPDS-01 can readily be downloaded in pdf format from a lot of places, but is over 70 MB. Official site for mil handbooks is
http://assist.daps.dla.mil/online/start/ You have to register first at this site.