MIL-PRF-1/607D
TABLE I. Testing and inspection.
Inspection
Method
Notes
Test
Conditions
Symbol
Limits
Units
MIL-STD-
Min
Max
1311
Qualification inspection
Degradation due to
4021
---
---
---
---
---
---
vibration
Loaded Q
4461
2
---
QL
---
5.5
---
High-level VSWR
4474
---
2
---
---
1.15
---
Conformance inspection,
part 1
4
---
4482
2
---
F = Fo
b
-0.05
+0.05
---
Tuning susceptance
4486
2, 3
1
t
---
10
sec
Firing time
4488
2, 3
1
La
---
0.8
dB
Arc loss
1027
---
---
---
---
---
---
Temperature cycling
(nonoperating)
1027
---
50
---
Cycles
---
---
Temperature cycling
Group C
life test
Conformance inspection,
part 2
4101
---
---
---
---
---
---
Dielectric material strain
Hammer angle 25°
1036
1
---
---
---
---
---
Bump
Normalized conductance
4484
2
---
g
---
0.05
---
F = Fo
Conformance inspection,
part 3
4551
---
3
t
1,000
---
hrs
Group D
Life test
---
---
---
Life-test end points
4482
2
---
b
-0.05
+0.05
---
F = Fo
Tuning susceptance
4484
2
---
g
---
0.1
---
Normalized conductance
F = Fo
Firing time
4486
2, 3
1
t
---
10
sec
NOTES:
1.
The tube should not be hit directly with the hammer. An anvil as shown on Drawing 188-JAN may be used.
2.
Mount in accordance with Drawing 153-JAN, or equivalent.
3.
The tube shall be mounted as in note 2 and followed by a matched load. The tube shall fire within the limits specified after
application of rf power. This test shall be performed at least 7 days after pumping and at least 24 hours after any previous
discharge.
4.
This specification sheet uses accept on zero defect sampling in accordance with MIL-PRF-1, table III.
2
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