MIL-DTL-62006C(AT)
TABLE IV. Air and oil properties used in determining heat rejection.
Air
Oil
Static
Inlet
Outlet
Type,
Flow 1/
drop 1/
Inlet
Flow 1/
Pressure
tempera-
tempera-
gal/min
class
lb/min
in. H20
tempera-
Grade
drop psi
ture
ture
ture °F (°C)
°F (°C )
°F (°C )
(kPa)
(component)
(kg/min)
(SAE)
(L/min)
(kPa)
I,
A
170
11
140
15W-
150
30
---
300
(engine)
(77)
(2.7)
(60)
40
(567)
(210)
(149)
B and C
275
7.5
140
10W
284
30
225
---
(trans-
(125)
(1.9)
(60)
(1074)
(210)
(107)
mission)
II,
D
89
11
140
15W-
80
30
---
300
(engine)
(40)
(2.7)
(60)
40
(302)
(210)
(149)
(trans-
69
7.5
140
10W
78
25
225
---
mission)
(31)
(1.9)
(60)
(295)
(170)
(107)
II,
E
84
11
140
15W-
80
30
---
300
(engine)
(38)
(2.7)
(60)
40
(302)
(210)
(149)
(trans-
65
7.5
140
10W
78
25
225
---
mission)
(29)
(1.9)
(60)
(295)
(170)
(107)
III,
F&G
900
11
140
15W-
310
30
---
300
(engine)
(408)
(2.7)
(60)
40
(1172)
(210)
(149)
(trans-
900
7.5
140
10W
440
25
225
---
mission)
(408)
(1.9)
(60)
(1663)
(170)
(107)
1/ The following previously undefined abbreviations are used in this table: kg/min = kilograms
per minute, lb = pounds, and H20=water.
4.5 Support and ownership requirements verification. Complete each verification
under 4.5.
4.5.1 Hazardous material evaluation. Use one or more of the methods outlined in 4.3 to
verify that safety hazards are not present.
8
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