Q-Tech QT1C User Manual

INCH-POUND
MIL-PRF-55310/12H 11 June 2009
SUPERSEDING MIL-PRF-55310/12G 24 February 2005
OSCILLATOR, CRYSTAL CONTROLLED, TYPE 1 (CRYSTAL OSCILLATOR (XO)),
0.05 MHz THROUGH 10 MHz, HERMETIC SEAL, SQUARE WAVE, CMOS
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
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
Ltr
A --- .350 --- 8.89 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
.
Pin number Function 1 NC 2 NC 3 NC 4 B - (GND/CASE)
(See Note 5)
5 OUTPUT 6 NC 7 NC 8 B+
Inches mm
Min Max Min Max
.
AMSC N/A FSC 5955
MIL-PRF-55310/12H
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 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: -62C to +125C. Oscillator load: 10 kilohms 5 percent shunted by a 15 pF 5 percent capacitor for a CMOS compatible square
wave output. Output waveform: Symmetrical square wave. Supply voltage: See table I. Input current: At designated supply voltage (see table I). Output frequency: Frequency as designated at time of acquisition (see table I). Output voltage: Logic 1: See table I. Logic 0: See table I. Rise and fall times: See table I. Duty cycle: See table I. Initial accuracy at reference temperature: 25 ppm at +23C 1C up to 30 days after shipment. Initial frequency-temperature accuracy (one-half temperature cycle): Verification applicable. 1
-8
atm cc/s.
/
2
MIL-PRF-55310/12H
TABLE I. Dash numbers and operating characteristics.
Dash num-
ber
MHz V dc mA V dc V dc ns percent
01 .05 through 6 +15 35 13 2 30 40 to 60 02 6 through 10 +15 40 13 2 30 40 to 60 03 .05 through 6 +12 25 10 1 60 40 to 60 04 6 through 10 +12 30 10 1 60 40 to 60 05 .05 through 6 +10 20 9.5 0.5 60 40 to 60 06 6 through 10 +10 20 9.5 0.5 60 40 to 60
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
Frequency-voltage tolerance: 1 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.
5 ppm per year, maximum 0.7 ppm per 30 days. 1.5 ppm per 30 days
1.5 ppm per 90 days 3 ppm per 90 days Terminal strength: Method 211 of MIL-STD-202 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 Nonoperating: Test condition D. Operating: Not required. Ambient pressure: Nonoperating: In accordance with MIL-PRF-55310 Operating: Method 105 of MIL-STD-202
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 (f
Output
frequency
range
Supply
voltage
5%
Input
current
(max)
, test condition C.
ref
Output voltage Rise
Logic: 1
(min)
Logic: 0
(max)
and fall times (max)
Duty
cycle
-55C
+125C
A B C
100 70 55 100 70 55 100 70 55 100 70 55 100 70 55 100 70 55
/
10 ppm per year, maximum
, test condition C.
and method 204 of MIL-STD-202.
.
) instead of to the nominal frequency (f
nom
).
Frequency-temperature
tolerance (ppm)
to
-55C to
+105C
-20C
+70C
to
3
MIL-PRF-55310/12H
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
M55310/12-
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
MIL-STD-202
, this document references the following:
S 01 A XXXXXXXX
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: Preparing activity: Army - CR Army - CR Navy - EC Air Force - 99 Agent: DLA - CC DLA - CC
Review activities: (Project 5955-2009-013) Army - AR, MI, SM Navy - AS, CG, MC Air Force - 19, 84 NASA - NA
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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