HXNV0100AYN [HONEYWELL]

Memory Circuit, 64KX16, CMOS, CQFP64, QFP-64;
HXNV0100AYN
型号: HXNV0100AYN
厂家: Honeywell    Honeywell
描述:

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

内存集成电路
文件: 总12页 (文件大小:396K)
中文:  中文翻译
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HXNV0100  
HXNV0100 1Megabit  
64K x 16 Non-Volatile Magneto-Resistive RAM  
Features  
Fabricated on S150 Silicon On  
Insulator (SOI) CMOS Underlayer  
Technology  
150 nm Process (Leff = 130 nm)  
Total Dose Hardness 1x106 rad (Si)  
Dose Rate Upset Hardness 1x109  
rad(Si)/s  
Dose Rate Survivability 1x1012  
rad(Si)/s  
Soft Error Rate 1x10-10  
upsets/bit-day  
Neutron Hardness �1x1014 N/cm2  
No Latchup  
Read Access Time � 80 ns  
Read Cycle Time 110 ns  
Write Cycle Time 140 ns  
Typical Operating Power 500 mW  
Unlimited Read (>1x1015 Cycles)  
> 15 years Data Retention  
Synchronous Operation  
Single-Bit Error Detection &  
Correction (ECC)  
Dual Power Supplies  
1.8 V ± 0.15V, 3.3 V ± 0.3V  
3.3V CMOS Compatible I/O  
The 64K x 16 radiation hardened low power non-volatile Magneto-Resistive Random  
Access Memory (MRAM) is a high performance 65,536 word x 16-bit Magneto-Resistive  
RAM with industry-standard functionality.  
Standard Operating Temperature  
Range is -40°C to +105°C  
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  
Functional  
Block Diagram  
Digit Line Drivers  
A(7:15)  
Q
D
C
CS  
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(0:6)  
A(7:15)  
DQ(0:15)  
CS  
Definition  
Column Select Address Input. Signals which select a column within the memory array.  
Row Select Address Input. Signals which select a row within the memory array.  
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. The rising edge of CS will clock in the address and WE signals and latch the DQ outputs.  
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.  
WE  
OE  
NWI0  
NWI1  
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.  
NWI1 controls the upper order 32K A(15)=1.  
(Note the VIL and VIH requirements for NWI)  
TESTOUT  
TESTIN1  
TESTIN2  
TESTIN3  
VDD1  
This output signal is for Honeywell test purposes only. It must be left floating.  
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: 1.8V  
VDD2  
DC Power Source Input: 3.3V  
N/C  
No Connect, (can be tied to any supply)  
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 N/C  
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  
Signal Description  
Function Truth Table  
NWI  
CS  
OE  
WE  
Data Outputs  
Function  
1
_/  
X
1
X
1
Hi Z  
Write cycle  
(rising edge)  
X
0
_/  
(rising edge)  
X
0
X
Lo Z  
Read Cycle  
Dependent on controls  
Writes inhibited  
Output Driver Truth Table  
NWI  
CS  
0
OE  
X
WE(1)  
Data Outputs  
Hi Z  
Function  
X
X
X
X
X
X
1
0
Outputs Disabled  
Outputs Disabled  
Outputs Disabled  
Outputs Enabled  
X
0
Hi Z  
X
X
Hi Z  
1
1
Low Z  
(1) Latched by rising edge of CS  
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 will meet all stated functional and electrical  
specifications after the specified total ionizing radiation dose.  
All electrical and timing performance parameters will remain  
within specifications, post rebound, after an operational period  
of 15 years. Total dose hardness is assured by wafer level  
testing of process monitor transistors using 10 KeV X-ray.  
Parameter correlations have been made between 10 KeV X-rays  
applied at a dose rate of 5x105 rad(SiO2)/min at T= 25°C and  
gamma rays (Cobalt 60 source) to ensure that wafer level  
X-ray testing is consistent with standard military radiation  
test environments.  
SOI and Magnetic Memory Technology  
Transient Pulse Ionizing Radiation  
The MRAM is 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,  
when applied under recommended operating conditions.  
To ensure validity of all specified performance parameters  
before, during, and after radiation (timing degradation during  
transient pulse radiation is ±10%), it is suggested that stiffening  
capacitance be placed near the package VDD2 and ground  
(GND) and near the package VDD1 and ground (GND).  
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 150 nm process  
is a technology with a 31Å gate oxide for 1.8 V transistors and  
59Å gate oxide for 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 signal sensing,  
amplification, and readback. The resistance change from  
the memory element is a result of the change in Tunneling  
Magneto-Resistance (TMR) between the storage and pinned  
layers that depends on the magnetic state of the storage  
layer. The HXNV0100 is not subject to memory related wear  
out mechanisms.  
It is also recommended that the inductance between the MRAM  
package leads and the stiffening capacitance be less that 1.0 nH.  
If there are no operate through or valid stored-data requirements,  
typical circuit board mounted de-coupling capacitors are  
recommended. The MRAM will meet any functional or electrical  
specification after exposure to a radiation pulse up to the  
transient dose rate survivability specification, when applied  
under recommended operating conditions. Note that the current  
conducted during the pulse by the MRAM inputs, outputs, and  
power supply may significantly exceed the normal operating levels.  
The application design must accommodate these effects.  
Neutron Radiation  
The MRAM will meet any functional or timing specification after  
exposure to the specified neutron fluence under recommended  
operating or storage conditions. This assumes equivalent neutron  
energy of 1 MeV.  
Error Correction Code (ECC)  
Hamming 5-Bit ECC  
A 5-bit Hamming ECC is generated for all data written into  
memory. This code allows for the 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
Soft Error Rate  
Radiation-Hardness Ratings  
The MRAM is capable of meeting the  
specified Soft Error Rate (SER) under  
recommended operating conditions.  
This hardness level is defined by the  
Adams 90% worst case cosmic ray  
environment for geosynchronous orbits.  
Parameter  
Limits  
Units  
Test Conditions  
VDD1 = 1.65 TO 1.95 VOLTS  
VDD2 = 3.00 TO 3.60 VOLTS  
TC = -40 TO 105 °C  
6
Total Dose: H-Level  
1 x 10  
1 x 10  
1 x 10  
1 x 10  
Rads(Si)  
TA =25°C, X-Ray or Co60  
-10  
9
Soft Error Rate:  
Upsets/bit-day (1)  
Rads(Si)/s  
Read or Write  
Transient Dose Rate Upset  
Transient Dose Rate Survivability  
Neutron Fluence  
Pulse Width = 20ns +/- 5ns FWHM, X-Ray  
Pulse Width = 18-52ns FWHM, X-Ray  
1 MeV equivalent energy  
12  
Rads(Si)/s  
14  
2
1x10  
N/cm  
Latchup  
(1) Adams 90% Worst-Case environment under worst-case operating conditions for voltage, temperature and memory  
operating conditions (e.g. static or dynamic operation).  
The MRAM will not latch up under any  
of the above radiation exposure condi-  
tions when applied under recommended  
operating conditions. Fabrication with SOI  
substrate material provides oxide isolation  
between adjacent PMOS and NMOS  
transistors and eliminates any potential  
SCR-type latchup structures. Sufficient  
transistor body tie connections to the  
p-channel and n-channel substrates  
are made to ensure no source/drain  
snapback occurs.  
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  
Parameter  
Limits  
Units  
Test Conditions  
Magnetic Field  
50  
Oe  
VDD1 = 1.8 Volts, VDD2 = 3.3 Volts  
TC = -40°C to 105°C  
Recommended Operating Conditions (1)  
Limits  
Symbol  
VDD1  
Parameter  
Min  
1.65  
3.0  
Typical  
1.80  
3.3  
Max  
1.95  
Units  
Volts  
Volts  
°C  
Positive Supply Voltage  
Positive Supply Voltage  
External Package Temperature  
Voltage On Any Pin  
VDD2  
3.6  
T
-40  
25  
105  
C
V
-0.3  
VDD2+0.3  
Volts  
PIN  
(1) Voltages referenced to GND  
Electrical Specifications  
Absolute Maximum Ratings (1)  
Ratings  
Symbol  
VDD1  
Parameter  
Min  
Max  
2.5  
Units  
Volts  
Volts  
Volts  
°C  
Positive Supply Voltage (2)  
Positive Supply Voltage (2)  
Voltage on Any Pin (2)  
-0.5  
-0.5  
-0.5  
VDD2  
4.6  
V
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)  
D
Package Thermal Resistance (Junction to Case)  
Electrostatic Discharge Protection Voltage (4)  
Junction Temperature Silicon  
4.0  
°C /W  
V
JC  
V
2000  
PROT  
T
175  
160  
°C  
J
T
MTJ Temperature  
°C  
MTJ  
(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) Class 2 electrostatic discharge (ESD) input protection voltage per MIL-STD-883, Method 3015  
(5) Maximum soldering temp of 260°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)  
Capacitance  
Limits  
Symbol  
Parameter  
Min  
Max  
Units  
pF  
Test Conditions  
C
Data I/O Capacitance  
Input Capacitance  
15  
Vio = VDD2 or VSS, f=1 MHz  
VI = VDD2 or VSS, f=1 MHz  
IO  
C
12  
pF  
I
C
Not Write Inhibit Capacitance  
100  
pF  
NWI  
5
DC Electrical Characteristics (1)  
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)  
IDDOPWR1  
IDDOPWR7  
IDD2OPWR1  
IDD2OPWR7  
IDDOPR1  
VDD1 current at 1 MHZ write frequency  
(frequency of CS rising edges)  
15  
This is the average current comprised of 30 ma during  
each 140 ns internal MRAM write, and 12 ma standby  
in between each write  
VDD1 current at 7 MHZ write frequency  
(frequency of CS rising edges)  
30  
30  
196  
14  
30  
8
mA  
mA  
mA  
mA  
mA  
mA  
This is the average current comprised of 30 ma during  
each 140 ns internal MRAM write, and 12 ma standby  
in between each write  
VDD2 current at 1 MHZ of write frequency  
(frequency of CS rising edges)  
This is the average current comprised of 200 ma during  
each 140 ns internal MRAM write and 2 ma standby in  
between each write.  
VDD2 current at 7 MHZ of write frequency  
(frequency of CS rising edges)  
This is the average current comprised of 200 ma during  
each 140 ns internal MRAM write and 2 ma standby in  
between each write.  
VDD1 current at 1 MHZ of read frequency  
(frequency of CS rising edges)  
This is the average current comprised of 30 ma during  
each 110 ns internal MRAM read, and 12 ma standby in  
between each read  
IDDOPR9  
VDD1 current at 9 MHZ of read frequency  
(frequency of CS rising edges)  
This is the average current comprised of 30 ma during  
each 110 ns internal MRAM read, and 12 ma standby in  
between each read  
IDD2OPR1  
VDD2 current at 1 MHZ of read frequency  
(frequency of CS rising edges)  
Dynamic current is due to driving load capacitance,  
assumes all 16 outputs switching every read cycle  
I = 16 * C * V * F + standby current with 70 pF load  
per output  
IDD2OPR9  
VDD2 current at 9 MHZ of read frequency  
(frequency of CS rising edges)  
54  
mA  
Dynamic current is due to driving load capacitance,  
assumes all 16 outputs switching every read cycle  
I = 16 * C * V * F + standby current  
with 70 pF load per output  
(1) Post-radiation performance guaranteed at 25°C per MIL-STD-883 method 1019 up to 1MRad(Si) total dose  
6
Max Write Cycle IDDOP  
Max Read Cycle IDDOP  
250  
200  
150  
100  
50  
90.0  
80.0  
70.0  
60.0  
50.0  
40.0  
30.0  
20.0  
10.0  
0
IDDRD  
IDD2RD  
Total Read  
IDDWR  
IDDRWR  
Total Write  
0
0
2
4
6
8
0
2
4
6
8
10  
Frequency (MHz)  
Frequency (MHz)  
Data Endurance  
Ratings  
Parameter  
Min  
Max  
Units  
Cycles  
Cycles  
Test Conditions  
15  
Data Read Endurance  
Data Write Endurance  
1x10  
1x10  
12  
Data Retention  
Ratings  
Parameter  
Min  
Max  
Units  
Test Conditions  
Data Retention  
>15  
years  
Chip Power On or Off  
7
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  
Don’t Care  
Don’t Care  
Don’t Care  
ADDR Valid  
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  
ns  
Address Setup Time  
TADHD  
Address Hold Time  
15  
5
ns  
TWESU  
TWEHD  
TCSDV  
WE Setup Time  
ns  
WE Hold Time  
15  
ns  
DQ valid with respect to rising edge of CS  
OE access time  
80  
15  
15  
20  
ns  
TOEDV  
ns  
TOEHZ  
OE de-asserted to outputs Hi z  
CS de-asserted to outputs Hi z  
Read Cycle Time  
ns  
TCSHZ  
ns  
TMINR  
110  
ns  
TCSPI  
CS ignored pulse width (glitch tolerance)  
OE rising or falling edge to rising CS time  
CS rising edge to OE rising or falling edge  
4
ns  
TOENCBRCS  
TOENCARCS  
15  
65  
ns  
ns  
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  
Twehd  
ADD Valid  
Twesu  
Tnwisu  
Tnwi, Tnwihd  
NWI  
Name  
TADSU  
Description  
Min  
5
Max  
Units  
ns  
Address Setup Time  
Address Hold Time  
WE Setup Time  
WE Hold Time  
TADHD  
TWESU  
TWEHD  
TCSPW  
TCSPI  
15  
5
ns  
ns  
15  
10  
ns  
CS Pulse Width (for valid write)  
ns  
CS ignored pulse width (glitch tolerance)  
Data Setup Time (relative to CS rising edge)  
Data Hold Time (relative to CS rising edge)  
4
ns  
TDQSU  
TDQHD  
TNWI  
5
ns  
15  
ns  
NWI falling edge with respect to CS rising edge to inhibit write  
Write Cycle Time  
40  
ns  
TMINW  
140  
ns  
9
Power Up Timing  
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.  
• Utilizing a structured and controlled design process  
• A statistically controlled wafer fabrication process with  
a continuous defect reduction process  
• Individual wafer lot acceptance through process monitor testing  
(includes radiation testing)  
POWER UP SEQUENCE  
VDD1  
• The use of characterized and qualified packages  
• A thorough product testing program based on MIL-PRF-38535  
and MIL-STD 883.  
VDD2  
1us  
NWI  
Qualification and Screening  
The SOI CMOS technology is qualified by Honeywell after  
meeting the criteria of the General Manufacturing Standards  
and is also QML Qualified. This qualification is the culmination  
of years of development, testing, documentation, and on-going  
process control.  
Power Down Timing  
POWER DOWN SEQUENCE  
The test flow includes screening units with the defined flow  
(Class V and Q+ equivalent) and the appropriate periodic or lot  
conformance testing (Groups B, C, D, and E). Both the process  
and the products are subject to period or lot based Technology  
Conformance Inspection (TCI) and Quality Conformance  
Inspection (QCI) tests, respectively, as defined by Honeywell’s  
Quality Management Plan.  
VDD1  
VDD2  
100ns  
NWI  
Reliability  
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 first becoming QML qualified in 1990. 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 General  
Manufacturing Standards for:  
Group A  
Group B  
Final Lot Acceptance Electrical Tests  
Mechanical – Dimensions (1), Bond Strength, Solvents, Die Shear,  
Solderability, Lead Integrity, Seal, Acceleration  
Life Tests – 1000 hours at 105°C or equivalent  
Package related mechanical tests – Shock, Vibration, Accel, Salt (1),  
Seal, Lead Finish Adhesion, Lid Torque, Thermal Shock, Temp Cycle,  
Moisture Resistance  
Group C  
Group D  
Group E  
Radiation Tests  
• Designing in reliability by establishing electrical rules based  
on wear out mechanism characterization performed on  
specially designed test structures (electro migration, TDDB,  
hot carriers, negative bias temperature instability, radiation)  
(1) Testing performed by package supplier.  
10  
Package Outline  
The 64 Lead Shielded Ceramic QFP Package, including  
external capacitors. Magnetic shielding is tied to ground  
on the package.  
ꢂꢁ  
ꢛꢘꢜꢘꢈꢍ  
ꢄꢁꢘꢘꢘꢀ  
ꢍꢞ  
ꢉꢉ  
ꢉꢀ  
ꢍꢝ  
ꢕꢖꢗ  
ꢁꢇꢈꢉꢊ  
ꢋꢇꢌꢈꢍꢎ  
�ꢀ  
�ꢁ  
ꢂꢀ ꢂꢁ  
ꢏꢐꢑꢒꢓꢔ  
ꢈꢍ  
ꢁꢟ  
ꢁꢈ  
ꢉꢘꢘꢘꢜꢍ  
ꢃꢀ  
ꢃꢁ  
1. Controlling dimensions are in millimeters.  
Common Dimensions - Millimeters  
Common Dimensions - Inches  
Symbol  
Min  
3.86  
1.44  
0.41  
0.10  
22.63  
18.92  
---  
Nom  
4.29  
1.60  
0.46  
0.15  
22.86  
19.05  
1.27  
5.08  
---  
Max  
4.75  
1.76  
0.51  
0.20  
23.09  
19.18  
---  
Min  
.152  
.057  
.016  
.004  
.891  
.745  
---  
Nom  
.169  
.063  
.018  
.006  
.900  
.750  
.050  
.200  
---  
Max  
.187  
.070  
.020  
.008  
.909  
.755  
---  
2
A1 is the total thickness of the top shield,  
lid, sear ring, ceramic body, bottom  
shield, and shield adhesives.  
A
A1  
b
c
3
Lead frame corners are trimmed to fit  
into carriers.  
D1/E1  
D2/E2  
e
F
4.44  
---  
5.72  
52.58  
30.86  
---  
.175  
---  
.225  
2.070  
1.215  
---  
L1  
L2  
R
30.10  
8.03  
30.48  
---  
1.185  
.316  
1.200  
---  
11  
Ordering Information (1)  
H
X
NV  
0100  
A
Z
H
Source  
H = Honeywell  
Process  
X = SOI  
Part Type  
NV = Non Volatile  
Package Designation  
Total Dose Hardness  
6
A = 64 Lead QFP  
H = 1x10 rad (Si)  
N = No Level Guaranteed  
Part Number  
0100 = 1 Meg  
Screen Level  
Z = Class V Equivalent  
Y = Class Q+ 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  
QML Q+ Equivalent  
V Equivalent  
QCI Testing  
No lot specific testing performed. (2)  
Lot specific testing required in accordance with MIL-PRF-38535 Appendix B.  
(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.  
This product and related technical data is subject to the U.S. Department of State International Traffic in Arms Regulations (ITAR)  
22 CFR 120-130 and may not be exported, as defined by the ITAR, without the appropriate prior authorization from the Directorate of  
Defense Trade Controls, United States Department of State. Diversion contrary to U.S. export laws and regulations is prohibited.  
Honeywell reserves the right to make changes to improve reliability, function or design. Honeywell does not assume any liability  
arising out of the application or use of any product or circuit described herein; neither does it convey any license under its patent rights  
nor the rights of others.  
Find out more  
To learn more about Honeywell’s radiation hardened  
integrated circuit products and technologies, visit  
www.honeywell.com/microelectronics.  
Honeywell Aerospace  
Honeywell  
1944 E. Sky Harbor Circle  
Phoenix, AZ 85034  
Telephone: 1.800.601.3099  
N61-0995-000-000  
June 2010  
International: 602.365.3099  
www.honeywell.com  
© 2010 Honeywell International Inc.  

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