MIL-PRF-55310/9J - Vectron International

INCH-POUND
MIL-PRF-55310/9J
11 June 2009
SUPERSEDING
MIL-PRF-55310/9H
24 February 2005
PERFORMANCE SPECIFICATION SHEET
OSCILLATOR, CRYSTAL CONTROLLED, TYPE 1 (CRYSTAL OSCILLATOR (XO)),
400 kHz THROUGH 60 MHz, HERMETIC SEAL, SQUARE WAVE, TTL
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
The requirements for acquiring the product described herein
shall consist of this specification sheet and MIL-PRF-55310.
Pin number
1
2
3
4
5
6
7
8
Function
NC
NC
NC
B - (GND/CASE)
(See note 5)
OUTPUT
NC
NC
B+
Inches
mm
Ltr
Min
Max
Min
Max
A
---
.300
---
7.62
B
.480
---
12.19
---
C
.016
.020
0.41
0.51
D
---
.040
---
1.02
E
---
.410
---
10.41
F
---
.330
---
8.38
G
.195
.205
4.95
5.21
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for general information only.
3. Standard marking, except omit Part or Identifying Number (PIN) this location.
4. Unless otherwise specified, tolerances are ±.005 (0.13 mm) for three place decimals and ±.02 (0.5 mm) for two
place decimals.
5. Case to be connected to base pin 4 to permit shielding of the oscillator.
6. All pins with NC function may be connected internally and are not to be used as external tie points or
connections.
7. Pin numbers shown on package are for reference only and need not appear on part.
FIGURE 1. Dimensions and configuration.
AMSC N/A
FSC 5955
MIL-PRF-55310/9J
REQUIREMENTS:
Interface and physical dimensions: See figure 1.
Mounting: See figure 1.
Terminals: See figure 1.
Seal: Hermetic in accordance with MIL-PRF-55310, maximum leakage rate 5 x 10-8 atm cc/s.
Weight: 0.175 ounce, maximum.
Oscillator: Class 2 or any class 1 or class 3 oscillator meeting all class 2 requirements and verification tests
specified herein and in MIL-PRF-55310.
Calibration: Manufacturer calibrated.
Screening: In accordance with MIL-PRF-55310, product level B or S, as applicable.
Temperature:
Operating: See table I.
Storage: -62C to +125C.
Oscillator load: See table I.
Output waveform: Symmetrical square wave.
Supply voltage: +5 V dc 10 percent.
Input current: At designated supply voltage (see table I).
Output frequency: Frequency as designated at time of acquisition (see table I).
Output voltage: At designated TTL load (see table I).
Logic 1: 2.4 V dc, minimum.
Logic 0: 0.5 V dc, maximum.
Rise and fall times: See table I.
Duty cycle: See table I.
Initial accuracy at reference temperature (up to 30 days after shipment): See table I.
Initial frequency-temperature accuracy (one-half temperature cycle): Verification applicable. 1/
Frequency-temperature tolerance (one-half temperature cycle, referenced to frequency measured at +23C 1C,
immediately prior to starting of the test): See table I. Measurements taken at ten equally spaced increments over
the specified operating temperature range. 1/
1/ For the purpose of transitioning this device to MIL-PRF-55310, ‘Frequency stability versus temperature’ has been
renamed ‘Frequency-temperature tolerance’. The verification requirements of ‘initial frequency-temperature
accuracy (one-half temperature cycle)’ shall apply except that frequency measurements shall be referenced to
the frequency measured at +23C 1C (fref) instead of to the nominal frequency (fnom).
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MIL-PRF-55310/9J
TABLE I. Dash numbers and operating characteristics.
Dash
number
01
05
11
15
21
25
Output
frequency
range
Input
current
max at
5.25 V
1%
1/
Pulse characteristics
Duty
cycle at
1.4 V
mA
Rise
and
fall
times
max
ns
400 kHz
to
9 MHz
50
15
45 to 55
10 TTL
50
15
45 to 55
10 TTL
9 MHz
to
25 MHz
30
15
40 to 60
10 TTL
30
15
40 to 60
10 TTL
25 MHz
to
60 MHz
50
5
40 to 60
6 TTL
50
5
40 to 60
6 TTL
Load
2/
Initial
accuracy
ppm at
+23C
1C
Frequency
aging
ppm/year
after 30
days
Frequency-temperature
tolerance (ppm)
-55C
-55C
-20C
to
to
to
+125C
+105C
+70C
A
percent
max
50
B


40
C


25
10
5
100
50
80
40
50
25
10
5
100
50
80
40
50
25


15
5
25
15
25
15
25
10
100
80
50
1/ Maximum input current for no load condition. Actual configuration of TTL loads must be added to determine
power supply requirements.
2/ A TTL unit load is defined as: 1.6 mA sink, 0.04 mA source, and 2 pF capacitance.
Frequency-voltage tolerance:  2 ppm maximum for a  10 percent change in supply voltage. Measurements
taken at reference temperature and operating temperature range end points.
Frequency aging: Measurements shall be taken at +70C  0.2C at intervals of not more than every 72 hours for a
minimum of 30 days (see table I).
5 ppm per year maximum
0.7 ppm per 30 days
1.5 ppm per 90 days
10 ppm per year maximum
1.5 ppm per 30 days
3 ppm per 90 days
Terminal strength: Method 211 of MIL-STD-202, test condition C.
Applied force: 2 pounds each terminal for 10 seconds.
Bends: Five at 45 degrees each.
Frequency-environmental tolerance: Not applicable.
Vibration, sinusoidal: In accordance with MIL-PRF-55310 and method 204 of MIL-STD-202.
Nonoperating: Test condition D.
Operating: Not required.
Ambient pressure:
Nonoperating: In accordance with MIL-PRF-55310.
Operating: Method 105 of MIL-STD-202, test condition C.
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MIL-PRF-55310/9J
Part or Identifying Number (PIN): Consists of "M" prefix followed by specification sheet number, a dash and coded
alphas, and numeric number. See example:
EXAMPLE
M55310/09-
S
01
A
XXXXXXXX
M prefix and specification sheet number
Product level (S, B, or C)
Dash number (see table I)
Operating temperature range
(A, B, or C) (see table I)
Frequency
Reference documents. In addition to MIL-PRF-55310, this document references the following:
MIL-STD-202
The margins of this specification are marked with vertical lines to indicate where changes from the previous issue
were made. This was done as a convenience only and the Government assumes no liability whatsoever for any
inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document
based on the entire content irrespective of the marginal notations and relationship to the last previous issue.
Custodians:
Army - CR
Navy - EC
Air Force - 99
DLA - CC
Preparing activity:
Army - CR
Review activities:
Army - AR, MI, SM
Navy - AS, CG, MC
Air Force - 19, 84
NASA - NA
(Project 5955-2009-010)
Agent:
DLA - CC
NOTE: The activities listed above were interested in this document as of the date of this document. Since
organizations and responsibilities can change, you should verify the currency of the information above using the
ASSIST Online database at http://assist.daps.dla.mil.
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