HXNV0100AZF [HONEYWELL]

Memory Circuit, 64KX16, CMOS, CQFP64, QFP-64;
HXNV0100AZF
型号: HXNV0100AZF
厂家: Honeywell    Honeywell
描述:

Memory Circuit, 64KX16, CMOS, CQFP64, QFP-64

内存集成电路
文件: 总11页 (文件大小:1407K)
中文:  中文翻译
下载:  下载PDF数据表文档文件
HXNV0100  
HXNV0100 1Megabit  
64K x 16 Non-Volatile Magneto-Resistive RAM  
Features  
n
Fabricated on S150 Silicon On  
Insulator (SOI) CMOS Underlayer  
Technology  
n
n
150 nm Process  
Total Dose Hardness 3x105 and  
1x106 rad (Si)  
Dose Rate Upset Hardness 1x109  
rad(Si)/s  
n
n
n
Dose Rate Survivability 1x1012 rad(Si)/s  
Soft Error Rate 1x10-10  
upsets/bit-day  
n
n
n
n
n
n
n
n
n
Neutron Hardness 1x1014 N/cm2  
No Latchup  
Read Access Time 80 ns  
Read Cycle Time 110 ns  
Write Cycle Time 140 ns  
Unlimited Read (> 1x1015 Cycles)  
15 years Data Retention  
Synchronous Operation  
Single-Bit Error Detection &  
Correction (ECC)  
n
n
n
n
Dual Power Supplies  
1.8 V 0.15V, 3.3 V 0.3V  
3.3V CMOS Compatible I/O  
The Honeywell 1 Megabit radiation hardened low power non-volatile Magneto-Resistive  
Random Access Memory (MRAM) offers high performance and is designed for space  
and military applications. The part is configured as a 65,536 word x 16 bit MRAM.  
Standard Operating Temperature  
Range is -40°C to +105°C  
n
Package: 64 Lead Shielded  
Ceramic Quad Flat Pack  
The MRAM is designed for very high  
reliability. Redundant write control lines,  
error correction coding and low-voltage  
write protection ensure the correct  
operation of the memory and protection  
from inadvertent writes.  
fabricated with Honeywell’s radiation  
hardened Silicon On Insulator (SOI)  
technology, and is designed for use in  
low-voltage systems operating in radiation  
environments. The MRAM operates over  
a temperature range of -40°C to +105°C  
and is operated with 3.3 ± 0.3V and  
1.8 ± 0.15V power supplies.  
Integrated Power Up and Power Down  
circuitry controls the condition of the  
device during power transitions. It is  
Simplified Functional  
Block Diagram  
Digit Line Drivers  
A(7:15)  
CS  
Q
D
C
Row  
Decoder  
Data Array  
65,536 x 16  
ECC Array  
65,536 x 5  
ECC Logic  
WE  
Q
D
C
NWI  
Bit Line Drivers  
OE  
Q
D
C
A(0:6)  
Column Decoder  
Data Input/Output  
Read Circuit  
Q
D
C
DQ(0:15)  
Signal Description  
Signal  
A(15:0)  
DQ(15:0)  
CS  
Definition  
A(15) is MSB, A(0) is LSB.  
Data Input/Output Signals. Bi-directional data pins which serve as data outputs during a read operation and as data inputs during a write operation.  
Chip select. Rising edge initiates an access of memory. A(15:0), WE and DQ(15:0) are latched on the rising edge. High level required for DQ(15:0)  
outputs to be enabled.  
WE  
Write Enable. Active high write enable. High state at rising edge of CS initiates a write cycle. Low state at rising edge of CS initiates a read cycle.  
Output Enable. Active high output enable. Low state puts outputs in high impedance state.  
Not Write Inhibit – When set low, these signals inhibit writes to the memory. A high level allows the memory to be written.  
NWI0 controls lower order 32K A(15)=0.  
OE  
NWI0  
NWI1  
NWI1 controls the upper order 32K A(15)=1.  
(Note the VIL and VIH requirements for NWI)  
TESTOUT  
TESTIN1  
TESTIN2  
TESTIN3  
TESTIN4  
VDD1  
This pin shall be treated as a “no connect” and have no connection on the circuit board.  
These signals are for Honeywell test purposes only. These must be grounded. (Failure to hold these pins low may result in  
permanent loss of functionality)  
DC Power Source Input: nominal 1.8V  
DC Power Source Input: nominal 3.3V  
VDD2  
2
Package  
Pinout  
VDD1  
GND  
1
2
3
4
5
6
7
8
9
48 VSS  
47 VDD2  
46 ADDR(6)  
45 ADDR(15)  
44 WE  
DQ(1)  
DQ(0)  
CS  
NWI(0)  
VDD2  
VDD1  
VSS  
43 TESTIN4  
42 OE  
41 VDD2  
40 VDD1  
39 VSS  
HXNV0100  
NWI(1) 10  
TESTIN3 11  
TESTOUT 12  
DQ(8) 13  
38 ADDR(14)  
37 ADDR(13)  
36 ADDR(12)  
35 ADDR(11)  
34 VSS  
DQ(9) 14  
VDD2 15  
VSS 16  
33 VDD1  
Function Truth Table  
NWI  
CS  
R
WE  
Function  
Write Cycle  
Read Cycle  
Write Inhibited  
1
X
0
1
0
1
R
R
Output Driver Truth Table  
Function  
CS  
1
OE  
1
Data Outputs  
Active  
Hi-Z  
Read Cycle  
Read Cycle  
Read Cycle  
Write Cycle  
Write Inhibited  
1
0
0
X
Hi-Z  
X
X
Hi-Z  
X
X
Hi-Z  
3
Radiation Characteristics  
RAM and ROM Functional Capability  
Total Ionizing Radiation Dose  
This MRAM incorporates two write control signals allowing the two  
sections of the memory to be controlled independently. The two  
NOT WRITE INHIBIT signals, NWI(0) and NWI(1), allow one section  
of the device to operate as a RAM and the other to operate as a  
ROM at the full control of the user. These signals should be hard  
wired to VDD2 or ground if active control is not needed. If control  
is desired, maximum 5K ohms pull up or down resistor should be  
used with care taken to insure that the VIH and VIL for the NWI  
pins are met.  
The MRAM has a radiation hardness assurance TID level of  
300 Krad(Si) and 1Mrad(Si), including overdose and  
accelerated annealing per MIL-STD-883 Method 1019. Total  
dose hardness is assured by qualification testing with a 60Co  
source and wafer level X-ray testing during manufacturing.  
Soft Error Rate  
Special process, cell, circuit and layout design considerations  
are included in the MRAM to minimize the impact of heavy ion  
and proton radiation and achieve a very low radiation induced  
Soft Error Rate (SER). Weibull parameters and other relevant  
attributes are available upon request to calculate projected upset  
rate performance for other orbits and environments.  
SOI CMOS and Magnetic Memory Technology  
Honeywell’s S150 Silicon On Insulator (SOI) CMOS is radiation  
hardened through the use of advanced and proprietary design,  
layout, and process hardening techniques. The S150 150 nm  
SOI CMOS process is a technology supporting 1.8 V and 3.3 V  
transistors. The memory element is a magnetic tunnel junction  
(MTJ) that is non-volatile and composed of a magnetic storage  
layer structure and a magnetic pinned layer structure separated  
by an insulating tunnel barrier. During a write cycle, the storage  
layer is written by the application of two orthogonal currents using  
row-and-column addressing. The resistance of the MTJ depends  
on the magnetic state of the storage layer structure, which uses  
the pinned layer structure as a reference, and which enables  
non-destructive signal sensing, amplification, and readback.  
The resistance change from the memory element is a result of  
the change in Tunneling Magneto-Resistance (TMR) in the MTJ  
that depends on the magnetic state of the storage layer.  
Transient Pulse Ionizing Radiation  
Many aspects of product design are addressed to handle  
the high energy levels associated with the transient dose events.  
This allows the MRAM to be capable of writing, reading, and  
retaining stored data during and after exposure to a transient  
ionizing radiation pulse, up to the specified transient dose rate  
upset specification.  
The MRAM will also meet functional and electrical specifications  
after exposure to a radiation pulse up to the transient dose rate  
survivability specification.  
Neutron Radiation  
SOI CMOS is inherently tolerant of neutron radiation. The  
MRAM meets functional and timing specifications after exposure  
to the specified neutron fluence, based on conventional neutron  
irradiation testing, on unpowered MRAM parts.  
Latchup  
Error Correction Code (ECC)  
The MRAM will not latch up due to any of the above radiation  
exposure conditions when applied under recommended operating  
conditions. Fabrication with the SOI CMOS substrate material  
provides oxide isolation between adjacent PMOS and NMOS  
transistors and eliminates any potential SCR latchup structures.  
attributes are available upon request to calculate projected upset  
rate performance for other orbits and environments.  
Hamming 5-Bit ECC  
A 5-bit Hamming ECC is generated for all data written into  
memory. This code allows for the detection and correction of all  
single-bit errors per address. On a read cycle, a data word is read  
from memory and corrected, if necessary, before being placed on  
the output data bus.  
There is no change made to the actual data in the memory cells  
based on the ECC results. Actual data in memory are changed  
only upon writing new values.  
4
Radiation-Hardness Ratings (1)  
Parameter  
Limits  
Units  
Environment Conditions  
6
Rads(Si)  
Total Dose: H-Level  
1 x 10  
5
F-Level  
3 x 10  
-10  
l Soft Error Rate (2):  
1 x 10  
Upsets/bit-day (1)  
Geosynchronous orbit during solar minimum non-flare conditions  
behind 100mil Aluminum shield  
Pulse Width 20nS  
9
Transient Dose Rate Upset  
Transient Dose Rate Survivability  
Neutron Fluence  
1 x 10  
1 x 10  
Rads(Si)/s  
Rads(Si)/s  
12  
Pulse Width 20nS  
14  
1x10  
2
N/cm  
1 MeV equivalent energy  
(1) Device will not latchup when exposed to any of the specified radiation environments.  
(2) Calculated using CREME96.  
Magnetic Field Characteristics  
The MRAM will meet all stated functional and electrical specifications over the entire operating temperature range when exposed to magnetic  
fields up to the rating supplied below. Exposure to larger magnetic fields may permanently affect functionality.  
Magnetic Field Rating (1)  
Parameter  
Limits  
Units  
Magnetic Field  
50  
Oe  
(1) Tested at 25°C  
Recommended Operating Conditions (1)(2)  
Limits  
Symbol  
VDD1  
Parameter  
Min  
1.65  
3.0  
Typical  
Max  
1.95  
Units  
Volts  
Volts  
°C  
Positive Supply Voltage  
Positive Supply Voltage  
External Package Temperature  
Voltage On Any Pin  
1.80  
3.3  
25  
VDD2  
3.6  
T
-40  
-0.3  
-55  
105  
C
V
VDD2+0.3  
105  
Volts  
°C  
PIN  
T
Storage Temperature  
25  
STORE  
(1) Voltages referenced to GND  
(2) Specifications listed in datasheet apply when operated under the Recommended Operating Conditions unless otherwise specified.  
Absolute Maximum Ratings (1)  
Ratings  
Symbol  
VDD1  
Parameter  
Min  
-0.5  
-0.5  
-0.5  
Max  
2.5  
Units  
Volts  
Volts  
Volts  
°C  
Positive Supply Voltage (2)  
VDD2  
Positive Supply Voltage (2)  
4.6  
V
Voltage on Any Pin (2)  
VDD2+ 0.5  
PIN  
T
Maximum Junction Temperature for Sustained Exposure  
Soldering Temperature  
125 (6)  
260°C  
2.5  
Exp  
T
°C *sec(5)  
W
SOLDER  
P
P
Package Power Dissipation (3)  
Package Thermal Resistance (Junction to Case)  
Electrostatic Discharge Protection Voltage (Human Body Model)  
Junction Temperature Silicon  
MTJ Temperature  
D
4.0  
°C /W  
V
JC  
V
2000  
PROT  
T
175  
160  
90  
°C  
J
T
°C  
MTJ  
OUT  
I
Max Output Current (7)  
mA  
(1) Stresses in excess of those listed above may result in immediate permanent damage to the device. These are stress ratings only, and operation at these levels is not implied.  
Frequent or extended exposure to absolute maximum conditions may affect device reliability.  
(2) Voltage referenced to VSS  
(3) MRAM power dissipation due to IDDS, IDDOP, and IDDSEI, plus MRAM output driver power dissipation due to external loading must not exceed this specification  
(4) Not applicable.  
(5) Maximum soldering temp of 250°C can be maintained for no more than 180 seconds over the lifetime of the part.  
(6) Not to exceed 24 hours duration (or equivalent at temperature using Ea = 1.235 eV)  
(7) Not to exceed 1 second  
Capacitance (1)  
Limit  
Symbol  
Parameter  
Max  
Units  
pF  
C
Data I/O Capacitance  
Input Capacitance  
15  
IO  
C
12  
pF  
I
Not Write Inhibit Capacitance  
100  
pF  
C
NWI(0),(1)  
(1) Maximum capacitance is verified as part of initial qualification only.  
5
DC Electrical Characteristics  
Parameter  
VIL  
Symbol  
Min  
Max  
Units  
Comments  
Low Level Input Voltage  
High-level Input Voltage  
Low Level Input Voltage (NWI Signals)  
High-level Input Voltage (NWI Signals)  
Low-level Output Voltage  
High-level Output Voltage  
Output Leakage Current  
0.3*VDD2  
V
V
V
All inputs except NWI  
All inputs except NWI  
NWI Inputs  
VIH  
0.7*VDD2  
0.9*VDD2  
VIL (NWI)  
VIH (NWI)  
VOL  
0.5  
0.5  
100  
10  
NWI Inputs  
V
V
IOL = 6 mA  
VOH  
VDD2-0.5  
-100  
IOH = -6 mA  
IOZ  
μA  
Chip deselected or output disabled  
(CS=0V, OE=0V)  
II  
Input Leakage Current  
-10  
μA  
IIL : Vin=0V, IIH : Vin=VDD2  
All inputs except TEST pins  
IDDSB  
Standby Current  
VDD1 (1.95V)  
12  
2
mA  
mA  
mA  
VDD2 (3.60V)  
IDDOPW1  
IDDOPW7  
IDD2OPW1  
IDD2OPW7  
IDDOPR1  
IDDOPR9  
IDD2OPR1  
IDD2OPR9  
VDD1 current at 1 MHZ write frequency  
(frequency of CS rising edges)  
VDD1 current at 7 MHZ write frequency  
(frequency of CS rising edges)  
VDD2 current at 1 MHZ of write frequency  
(frequency of CS rising edges)  
VDD2 current at 7 MHZ of write frequency  
(frequency of CS rising edges)  
VDD1 current at 1 MHZ of read frequency  
(frequency of CS rising edges)  
VDD1 current at 9 MHZ of read frequency  
(frequency of CS rising edges)  
VDD2 current at 1 MHZ of read frequency  
(frequency of CS rising edges)  
VDD2 current at 9 MHZ of read frequency  
(frequency of CS rising edges)  
15  
30  
30  
196  
14  
30  
8
mA  
mA  
mA  
mA  
mA  
mA  
mA  
54  
Data Endurance  
Ratings  
Min  
Parameter  
Units  
15  
Data Read Endurance  
Data Write Endurance  
1x10  
Cycles  
Cycles  
15  
1x10  
Data Retention  
Ratings  
Parameter  
Min  
Max  
Units  
Conditions  
Chip Power On or Off  
Data Retention  
15  
years  
6
Read Cycle  
The MRAM is synchronous in operation relative to the rising edge  
of the Chip Select (CS) signal. With the initiation of a CS signal,  
the address and the Write Enable (WE) signal are latched into the  
device and the read operation begins. The memory locations are  
read and compared with the ECC values. Any single bit errors are  
detected and corrected.  
If WE was low when latched in, the data word is sent to the output  
drivers. In addition to WE low being latched, Output Enable (OE)  
must be set to a high value to enable the DQ output buffers. OE  
is not latched, and may be set high before or after the rising edge  
of CS.  
Read Cycle AC Timing Characteristics  
Tminr  
CS  
Tcspi  
Tadsu  
Tadhd  
Twehd  
ADDR Valid  
ADDR  
Don’t Care  
Don’t Care  
Don’t Care  
Twesu  
WE  
Don’t Care  
Tcsdv  
DQ = HiZ or Prev. Read Data  
Tcshz  
DQ = HiZ  
DQ Valid  
DQ = HiZ  
Toencbrcs  
Toencarcs  
Toedv  
Toehz  
See Note 1  
OE  
Don’t Care  
(1) If OE is held high during no change window (Toencbrcs+Toencarcs), the DQ pins will drive the previously read data after rising CS.  
If OE is held low during no change window, the DQ pins will remain at HiZ.  
Name  
TADSU  
Description  
Min  
5
Max  
Units  
Address Setup Time  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
TADHD  
Address Hold Time  
15  
5
TWESU  
TWEHD  
TCSDV  
WE Setup Time  
WE Hold Time  
15  
DQ valid with respect to rising edge of CS  
OE access time  
80  
15  
15  
20  
TOEDV  
TOEHZ  
OE de-asserted to outputs Hi z  
CS de-asserted to outputs Hi z  
Read Cycle Time  
TCSHZ  
TMINR  
110  
TCSPI  
CS ignored pulse width (glitch tolerance)  
OE rising or falling edge to rising CS time (1)  
CS rising edge to OE rising or falling edge (1)  
4
TOENCBRCS  
TOENCARCS  
15  
65  
(1) Guaranteed by design, not tested.  
(2) The timing specifications are referenced to the Timing Input / Output References diagrams and the Timing Reference Load Circuit diagrams.  
IBIS models should be used to evaluate timing under application load and conditions.  
8
Write Cycle  
The MRAM is synchronous in operation relative to the rising edge  
of the Chip Select (CS) signal. With the initiation of a CS signal,  
the address and the Write Enable (WE) signal are latched into  
the device.  
The bit cell construction of this device does not provide a method  
of simply writing a “1” or a “0” to match the data. The “write” to  
a bit can only change its state, thus the need to read the bit  
locations first. Only the bits which need to “change state” are  
actually written.  
The WRITE CYCLE begins by reading the currently addressed  
value in memory. The current memory data are compared to  
the data to be written. If the location needs to change value,  
the data are then written.  
Write Cycle AC Timing Characteristics  
Tminw  
Tcspw, Tcspi  
CS  
Tdqsu  
Tdqhd  
DQ Valid  
Data Written  
DQ = HiZ  
ADDR  
WE  
Tadsu  
Tadhd  
ADDR Valid  
Twesu  
Twehd  
Tnwisu  
NWI  
Tnwihd  
Tnwihd  
To use NWI to inhibit a  
WRITE operation  
NWI  
Tnwisu  
Name  
TADSU  
Description  
Min  
5
Max  
Units  
ns  
Address Setup Time  
Address Hold Time  
WE Setup Time  
WE Hold Time  
4
TADHD  
TWESU  
TWEHD  
TCSPW  
TCSPI  
15  
5
ns  
ns  
15  
10  
ns  
CS Pulse Width (for valid write)  
CS ignored pulse width (glitch tolerance)  
Data Setup Time (relative to CS rising edge)  
Data Hold Time (relative to CS rising edge)  
NWI Setup Time  
ns  
ns  
TDQSU  
TDQHD  
TNWISU  
TNWIHD  
TMINW  
5
ns  
15  
-40  
140  
140  
ns  
ns  
NWI Hold Time  
ns  
Write Cycle Time  
ns  
(1) The timing specifications are referenced to the Timing Input / Output References diagrams and the Timing Reference Load Circuit diagrams.  
IBIS models should be used to evaluate timing under application load and conditions.  
9
Power Up Timing  
Screening and Conformance Inspection  
The product test flow includes screening units with the applicable  
flow (Engineering Model, QML V, QML Q, Class V and Q equivalent)  
and the appropriate periodic or lot conformance testing (Groups A,  
B, C, D, and E). Both the wafer process and the products are  
subject to periodic or lot based Technology Conformance  
Inspection (TCI) and Quality Conformance Inspection (QCI)  
tests as defined by Honeywell’s Quality Management Plan.  
During power-up there are no restrictions on which supply  
comes up first provided NWI is asserted (low). NWI is de-asserted  
within 1us of both supplies reaching their 90% values.  
POWER UP SEQUENCE  
VDD1  
VDD2  
1us  
Conformance Summary  
NWI  
Group A  
Group B  
General Electrical Tests  
Mechanical – Resistance to Solvents, Bond Strength, Die Shear,  
Solderability  
Power Down Timing  
Group C  
Group D  
Life Tests – 1000 hours at 125°C or equivalent  
Package related mechanical tests – Physical Dimensions, Lead Integrity,  
Thermal Shock, Temp Cycle, Moisture Resistance, Seal, Mechanical  
Shock, Vibration, Acceleration, Salt Atmosphere, Internal Water Vapor,  
Adhesion of Lead Finish  
POWER DOWN SEQUENCE  
Group E  
Radiation Tests  
VDD1  
AC Timing Input and Output References  
VDD2  
100ns  
VIHac  
90%  
10%  
90%  
10%  
Input  
Levels(1)  
NWI  
VREF(2)  
VILac  
Reliability  
VREF(2)  
For many years Honeywell has been producing integrated circuits  
that meet the stringent reliability requirements of space and defense  
systems. Honeywell has delivered hundreds of thousands of QML  
parts since the early 1990’s. Using this proven approach Honeywell  
will assure the reliability of the products manufactured with the SOI  
CMOS process technology. This approach includes adhering to  
Honeywell’s Quality Management Plan for:  
Output  
Sense  
Levels  
VOHss-0.1V(2,3)  
VOLss+0.1V(2,3)  
High-Z(4)  
VOHss-0.1V(2,3)  
VOLss+0.1V(2,3)  
High-Z(4)  
Notes:  
• Designing in reliability by establishing electrical rules based on  
wear out mechanism characterization performed on specially  
designed test structures (electromigration, TDDB, hot carriers,  
bias temperature instability and radiation).  
(1) All input rise and fall times =1ns between the 90% and 10% levels.  
(2) Timing parameters reference voltage level.  
(3) ss: Low_Z VOH and VOL steady-state output voltage.  
(4) High-Z output pin pulled to VDD2 by Output Load Circuit.  
I/O Type  
VIHac  
VDD2  
VILac  
VSS  
VREF  
• Utilizing a structured and controlled design process.  
3.3V CMOS  
VDD2/2  
• Statistically controlling wafer fabrication process with a  
continuous defect reduction process.  
AC Timing Output Load Circuit  
• Performing individual wafer lot acceptance through process  
monitor testing (includes radiation testing).  
VLOAD  
• Using characterized and qualified packages.  
50 ohms  
• Performing thorough product testing program based on  
MIL-PRF-38535 and MIL-STD 883.  
DUT  
Output  
o
o
Zo=50 ohms  
o
30pF (1)  
Notes:  
(1) Set to 5pF for T*QZ (Low-Z to High-Z)  
timing parameters  
I/O Type  
VLOAD  
3.3V CMOS  
VDD2/2  
10  
Package Outline  
The 64 Lead Shielded Ceramic QFP Package, including  
external capacitors. Magnetic shielding is tied to ground  
on the package.  
L1  
A
2
b x 64  
R
A1  
48  
33  
32  
49  
Pkg  
X
C
L
4
E2  
E1  
L2 L1  
E4  
3
E3  
TOP  
SHIELD  
Cavity  
BOTTOM  
SHIELD SQ  
C
L
64  
17  
1
16  
e
F
c
D2  
D1  
Controlling dimensions are in millimeters.  
1.  
2
Common Dimensions - Millimeters  
Common Dimensions - Inches  
Symbol  
Min  
Nom  
Max  
Min  
Nom  
Max  
A is the total thickness of the top shield,  
lid, seal ring, ceramic body, bottom  
4.34  
3.85  
4.83  
.151  
.171  
.190  
A
A1  
b
1.44  
0.41  
1.60  
0.46  
1.76  
0.51  
.057  
.016  
.004  
.891  
.063  
.018  
.006  
.900  
.750  
.525  
.800  
.070  
.020  
.008  
.909  
.755  
.530  
.805  
.055  
shield, and shield adhesives.  
c
0.10  
0.15  
0.20  
3
No edge of the shield shall extend past  
the outer edge of the lid flange.  
D1/E1  
D2/E2  
E3  
E4  
e
22.63  
18.92  
13.21  
22.86  
19.05  
13.34  
23.09  
19.18  
13.46  
.745  
.520  
.795  
20.19  
1.14  
4.44  
---  
20.32  
1.27  
5.08  
20.45  
1.40  
All edges of the bottom shield shall  
be a minimum of 0.030" to the edge  
of the ceramic body.  
4
.050  
.200  
---  
.045  
.175  
5.72  
.225  
F
L1  
---  
---  
2.060  
52.32  
L2  
R
1.185  
.316  
---  
1.200  
---  
30.10  
8.03  
---  
1.215  
---  
30.48  
---  
30.86  
---  
.066  
---  
X
---  
1.687  
11  
Ordering Information (1)  
H
Source  
X
NV  
Part Type  
0100  
A
Z
H
Total Dose Hardness  
Process  
X = SOI  
Package Designation  
6
H = 1x10 rad (Si)  
H = Honeywell  
NV = Non Volatile  
A = 64 Lead QFP  
F = 3x105 rad (Si)  
N = No Level Guaranteed  
Part Number  
0100 = 1 Meg  
Screen Level  
Z = Class V Equivalent  
E = Eng. Model (2)  
(1) To order parts or obtain technical assistance, call 1-800-323-8295  
(2) Engineering Model Description: Parameters are tested from -40°C to 105°C, 24-hour burn-in, no radiation guarantee.  
QCI Testing (1)  
Classification  
QCI Testing  
Lot specific testing required in accordance with MIL-PRF-38535 Appendix B.  
V Equivalent  
(1) QCI groups, subgroups and sample sizes are defined in MIL-PRF38535 and the Honeywell QM Plan. Quarterly testing is done in accordance with the Honeywell QM Plan.  
(2) If customer requires lot specific testing, the purchase order must indicate specific tests and sample sizes.  
Honeywell reserves the right to make changes of any sort without notice to any and all products, technology and testing identified herein.  
You are advised to consult Honeywell or an authorized sales representative to verify that the information in this data sheet is current before  
ordering this product. Absent express contract terms to the contrary, Honeywell does not assume any liability of any sort arising out of  
the application or use of any product or circuit described herein; nor does it convey any license or other intellectual property rights of  
Honeywell or of third parties.  
Find out more  
To learn more about Honeywell’s radiation hardened  
integrated circuit products and technologies, visit  
www.honeywell.com/microelectronics.  
Honeywell Aerospace  
Honeywell  
12001 Highway 55  
Plymouth, MN 55441  
ADS-14191 Rev. B  
March 2015  
Tel: 800-323-8295  
© 2015 Honeywell International Inc.  
www.honeywellmicroelectronics.com/  

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