DS16F95QML

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SNOSAN0B – SEPTEMBER 2005 – REVISED APRIL 2013

DC - Receiver Electrical Characteristics

(1) (continued)

Symbol

Parameter

Conditions

Notes

Min

Max

Unit

Sub-group

Output Short Circuit

-85

-15

mA

1, 2, 3

.2

V

1, 2, 3

Differential Input High

Threshold

.2

V

1, 2, 3

-.2

V

1, 2, 3

Differential Input Low

Threshold

-.2

V

1, 2, 3

35

mV

1, 2, 3

Hyteresis

35

mV

1, 2, 3

DC - Both Driver and Receiver Electrical Characteristics

(1)

Symbol

Parameter

Conditions

Notes

Min

Max

Unit

Sub-group

RE = 2V, DE = .8V

25

mA

1, 2, 3

RE =.8V, DE = 2V

28

mA

1, 2, 3

Input Clamp Volt

-1.3

V

1, 2, 3

Logical "1" Input Voltage

2

V

1, 2, 3

Logical "0" Input Voltage

.8

V

1, 2, 3

Logical "1" Enable Input Voltage

2

V

1, 2, 3

Logical "0" Enable Input Voltage

.8

V

1, 2, 3

Logical "0" Input Current

-50

uA

1, 2, 3

(1)

Pre and post irradiation limits are identical to those listed under A C and DC electrical characteristics. These parts may be dose rate

sensitive in a space environment and demonstrate enhanced low dose rate effect. Radiation end point limits for the noted parameters

are ensured only for the conditions as specified in MIL-STD 883, Method 1019, condition A.

(2)

Negative sign of the limits indicates the direction of the current flow only.

AC - Driver Electrical Characteristics

(1)

The following conditions apply to all parameters, unless otherwise specified.

Symbol

Parameter

Conditions

Notes

Min

Max

Unit

Sub-group

Differential Output Delay Time

8

25

nS

9

(See Figure 6)

8

30

nS

10, 11

Differential Output Transition

8

25

nS

9

Time (See Figure 6)

8

30

nS

10, 11

Propagation Delay Time Low to

6

18

nS

9

High (See Figure 7)

6

25

nS

10, 11

Propagation Delay Time high to

6

18

nS

9

Low (See Figure 7)

6

25

nS

10, 11

Output Enable Time to H

35

nS

9

(See Figure 8)

45

nS

10, 11

Output Enable Time to L

40

nS

9

(See Figure 9)

50

nS

10, 11

(1)

Pre and post irradiation limits are identical to those listed under A C and DC electrical characteristics. These parts may be dose rate

sensitive in a space environment and demonstrate enhanced low dose rate effect. Radiation end point limits for the noted parameters

are ensured only for the conditions as specified in MIL-STD 883, Method 1019, condition A.

(2)

Rise time 20% to 80%, Fall time 80% to 20%.

(3)

tTD = Non-inverting output rise time + inverting output fall time / 2, Non-inverting output fall time + inverting output rise time / 2.

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