SMFLHP2805S [CRANE]

Parallel operation with current share, up to 3 units (228 watts); 并行操作,目前的股价,最多3个单位(228瓦)
SMFLHP2805S
型号: SMFLHP2805S
厂家: Crane Aerospace & Electronics.    Crane Aerospace & Electronics.
描述:

Parallel operation with current share, up to 3 units (228 watts)
并行操作,目前的股价,最多3个单位(228瓦)

文件: 总13页 (文件大小:465K)
中文:  中文翻译
下载:  下载PDF数据表文档文件
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Features  
Parallel operation with current share,  
up to 3 units (228 watts)  
•ꢀ -55° to +125°C operation  
•ꢀ 19 to 40 VDC input  
•ꢀ 50 V for 120 ms transient protection  
•ꢀ Fully isolated, magnetic feedback  
•ꢀ Fixed high frequency switching  
•ꢀ Remote sense or output trim on single output models  
•ꢀ Inhibit function  
•ꢀ Synchronization input and output  
•ꢀ Indefinite short circuit protection  
models  
VDC Ou t p u t  
•ꢀ High power density with up to 87% efficiency  
SINꢀLE  
3.3  
5
DꢁAL  
±5  
±12  
±15  
12  
15  
description  
Tight load regulation is achieved through a wide-bandwidth  
magnetic feedback circuit. The output voltage on single SMFLHP  
models can be easily trimmed up by adding an external resistor.  
(See Figure 2 for voltage changes with different resistor values.)  
The SMFLHP Series™ 28 volt DC/DC converters are rated up  
to 100 watts output power over a –55°C to +125°C temperature  
range with a 28 VDC nominal input. On dual output models, up to  
70% of the rated output power can be drawn from either the posi-  
tive or negative outputs. Current sharing allows the units to be  
paralleled for total power of up to 228 watts. The welded, hermet-  
ically sealed package is only 3.005 x 1.505 x 0.400 inches, giving  
the series an overall power density of up to 67 watts per cubic  
inch.  
in h i b i t  
The SMFLHP Series converters have two inhibit terminals  
(INH1 and INH2) that can be used to disable power conversion,  
resulting in a very low quiescent input current. A low (<0.8 volts)  
is required between INH1 (pin 4) and Input Common (pin 2) to  
inhibit the converter. A low (<0.5 volts) is required between INH2  
(pin 12) and Output Common (pin 8) to inhibit the converter. The  
application of intermediate voltages to these pins (1.5 to 10.5  
volts) should be avoided.  
Sc r e e n i n g  
SMFLHP converters offer screening options to Space Prototype  
(O), Class H, or Class K. Radiation tolerant to Radiation  
Hardness Assurance (RHA) levels of “-” (O), “P” or “R”, per MIL-  
STD-38534. Interpoint model numbers use an “O” in the RHA  
designator position to indicate the “-” (dash) Radiation Hardness  
Assurance level of MIL-PRF-38534, which is defined as “no  
RHA”. See “Class H and K, QML Screening” tables for more  
information.  
cu r r e n t Sh a r i n g a n D Pa r a l l e l OP e r a t i O n  
Multiple SMFLHP converters may be used in parallel to drive a  
common load (see Figure 3). In this mode of operation the load  
current is shared by two or three SMFLHP converters. In current  
sharing mode, one SMFLHP converter is designated as a master.  
The SLAVE pin (pin 11) of the master is left unconnected and  
the MSTR/INH2 pin (pin 12) of the master is connected to the  
SLAVE pin (pin 11) of the slave units. The units designated as  
slaves have the MSTR/INH2 pin (pin 12) connected to the SNS  
RTN pin (pin 9) of the master unit. Figure 3 shows the typical  
setup for two or three units in parallel. Note that synchronizing  
the units together (though shown in the figure) is not required for  
current sharing operation. A second slave unit may be placed in  
parallel with a master and slave; this requires the TRI pin (pin 3)  
of the master unit to be connected to the SNS RTN pin (pin 9).  
De S i g n Fe a t u r e S  
The SMFLHP Series converters are switching regulators that use  
a quasi-square wave, single ended forward converter design with  
a constant switching frequency of 600 kHz.  
Isolation between input and output circuits is provided with a  
transformer in the forward path and wide bandwidth magnetic  
coupling in the feedback control loop. The SMFLHP Series  
uses a unique dual loop feedback technique that controls output  
current with an inner feedback loop and output voltage with a  
cascaded voltage mode feedback loop.  
When paralleled, 76% of the total combined power ratings of the  
SMFLHP converters are available at the load. Overload and short  
circuit performance are not adversely affected during parallel  
operation.  
The additional secondary current mode feedback loop improves  
transient response in a manner similar to primary current mode  
control and allows for ease of paralleling.  
Crane Aerospace & Electronics  
Page 1 of 13  
Electronics ꢀroup (Interpoint Brand)  
POꢀBoxꢀ97005ꢀꢀ•ꢀꢀRedmondꢀWAꢀ98073-9705  
425.882.3100ꢀꢀꢀ•ꢀꢀꢀelectronics@craneae.com  
www.craneae.com  
Rev H - 20071221  
Cleared by ꢁ.S. DoD OSR for Public Release  
OSR case number 09S-0995, dated March 13, 2009.  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Operating COnditiOns and CharaCteristiCs  
synC in and inhibit (inh1, inh2)  
iꢁꢋꢆꢉ Vꢇꢂꢉꢄgꢃ rꢄꢁgꢃ  
syꢁꢍ iꢁ (525 ꢉꢇ 675 kHz)  
ꢀ •ꢀ19ꢀtoꢀ40ꢀVDCꢀcontinuousꢀ  
ꢀ •ꢀ50ꢀVꢀforꢀ50ꢀmsecꢀtransient  
oꢆꢉꢋꢆꢉ pꢇwꢃꢈ  
ꢀ •ꢀupꢀtoꢀ100ꢀwattsꢀdependingꢀonꢀmodel  
lꢃꢄꢅ sꢇꢂꢅꢃꢈꢀꢁg tꢃꢌꢋꢃꢈꢄꢉꢆꢈꢃ (10 ꢊꢃꢍ ꢋꢃꢈ ꢂꢃꢄꢅ)  
ꢀ •ꢀ300°C  
ꢀ •ꢀDutyꢀcycleꢀ40%ꢀmin,ꢀ60%ꢀmaxꢀ  
ꢀ •ꢀLogicꢀlowꢀ0.8ꢀVꢀmax  
ꢀ •ꢀLogicꢀhighꢀ4.5ꢀVꢀmin,ꢀ5ꢀVꢀmax  
ꢀ •ꢀReferencedꢀtoꢀinputꢀcommon  
ꢀ •ꢀIfꢀnotꢀused,ꢀconnectꢀtoꢀinputꢀcommon  
sꢉꢇꢈꢄgꢃ tꢃꢌꢋꢃꢈꢄꢉꢆꢈꢃ rꢄꢁgꢃ (cꢄꢊꢃ)  
ꢀ •ꢀ–65°Cꢀtoꢀ+150°C  
syꢁꢍ oꢆꢉ  
ꢀ •ꢀReferencedꢀtoꢀinputꢀcommon  
pꢇwꢃꢈ dꢀꢊꢊꢀꢋꢄꢉꢀꢇꢁ (pꢅ)  
ꢀ •ꢀ20ꢀwattsꢀ  
iꢁhꢀbꢀꢉ (inH1, inH2) oꢋꢃꢁ cꢇꢂꢂꢃꢍꢉꢇꢈ  
ꢀ •ꢀLogicꢀlowꢀ(outputꢀdisabled)  
Current –10 to –5 mA  
cꢄꢊꢃ oꢋꢃꢈꢄꢉꢀꢁg tꢃꢌꢋꢃꢈꢄꢉꢆꢈꢃ (tꢍ)  
ꢀ •ꢀ–55ꢀtoꢀ+125°Cꢀfullꢀpower  
ꢀ •ꢀ–55ꢀtoꢀ+135°Cꢀabsolute  
dꢃꢈꢄꢉꢀꢁg oꢆꢉꢋꢆꢉ pꢇwꢃꢈ/cꢆꢈꢈꢃꢁꢉ  
ꢀ •ꢀLinearlyꢀfromꢀ100%ꢀatꢀ125°Cꢀtoꢀ0%ꢀatꢀ135°C  
oꢆꢉꢋꢆꢉ Vꢇꢂꢉꢄgꢃ tꢃꢌꢋꢃꢈꢄꢉꢆꢈꢃ cꢇꢃffꢀꢍꢀꢃꢁꢉ  
ꢀ •ꢀ100ꢀppm/°Cꢀtypical  
INH1 referenced to input common  
Logic low 0.8 V max  
INH2 referenced to output common  
Logic low 0.5 V max  
ꢀ •ꢀLogicꢀhighꢀ(outputꢀenabled)  
Open collector  
iꢁꢋꢆꢉ ꢉꢇ oꢆꢉꢋꢆꢉ cꢄꢋꢄꢍꢀꢉꢄꢁꢍꢃ  
ꢀ •ꢀ150ꢀpFꢀtypical  
iꢊꢇꢂꢄꢉꢀꢇꢁ  
ꢀ •ꢀ100ꢀmegohmꢀminimumꢀatꢀ500ꢀVDC,ꢀanyꢀpinꢀtoꢀcase  
aꢆꢅꢀꢇ rꢃjꢃꢍꢉꢀꢇꢁ  
ꢀ •ꢀ50ꢀdBꢀtypical  
cꢇꢁvꢃꢈꢊꢀꢇꢁ Fꢈꢃqꢆꢃꢁꢍy  
ꢀ •ꢀFreeꢀrunꢀmodeꢀ600ꢀkHzꢀtypical  
550 kHz min, 650 kHz. max  
ꢀ •ꢀExternalꢀsyncꢀrangeꢀ525ꢀtoꢀ675ꢀkHz  
iꢁhꢀbꢀꢉ pꢀꢁ Vꢇꢂꢉꢄgꢃ (ꢆꢁꢀꢉ ꢃꢁꢄbꢂꢃꢅ)  
ꢀ •ꢀINH1ꢀ=ꢀ9ꢀto12ꢀV,ꢀINH2ꢀ=ꢀ6ꢀtoꢀ9ꢀV  
meChaniCal and envirOnmental  
sꢀzꢃ (ꢌꢄxꢀꢌꢆꢌ)  
3.005 x 1.505 x 0.400 inches (76.33 x 38.23 x 10.16 mm)  
See case ꢁ for dimensions.  
Wꢃꢀghꢉ (ꢌꢄxꢀꢌꢆꢌ)  
86 grams  
sꢍꢈꢃꢃꢁꢀꢁg  
Space Prototype (O), Class H, or Class K Radiation tolerant to Radiation Hardness Assurance (RHA) levels of “-” (O), “P” or “R”, per  
MIL-STD-38534. Interpoint model numbers use an “O” in the RHA designator position to indicate the “-” (dash) Radiation Hardness  
Assurance level of MIL-PRF-38534, which is defined as “no RHA”.  
See “Class H and K, QML Screening” tables for more information.  
Available configurations: OO, HO, HP, HR, KR  
www.craneae.com  
Page 2 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
pins nOt in Use  
pin OUt  
pꢀꢁ sꢀꢁꢂꢃꢄ Ouꢅꢆuꢅ  
duꢇꢃ Ouꢅꢆuꢅ  
tr1  
Leave unconnected  
Leave unconnected  
Leave unconnected  
Connect to input common  
Must be connected to appropriate  
outputs  
1
2
3
4
5
6
7
8
9
Positive Input  
Input Common  
Triple (TRI)  
Inhibit 1 (INH1)  
Sync Out  
Sync In  
Positive Output  
Output Common  
Sense Return  
Positive Input  
Input Common  
Triple (TRI)  
Inhibit 1 (INH1)  
Sync Out  
iꢁhꢀbꢀꢉ (inH1)  
syꢁꢍ oꢆꢉ  
syꢁꢍ iꢁ  
sꢃꢁꢊꢃ lꢀꢁꢃꢊ  
sꢂꢄvꢃ  
mstr (inH 2)  
Leave unconnected  
Leave unconnected  
Sync In  
Positive Output  
Output Common  
Negative Output  
No connection  
Slave  
10 Positive Sense  
11 Slave  
12 Master / Inhibit 2  
(MSTR/INH2)  
Master / Inhibit 2  
(MSTR/INH2)  
Angled corner indicates pin one.  
1
2
12  
11  
10  
9
TOP VIEW  
SMFLHP  
(Pin side, marked side)  
3
4
5
6
8
See case ꢁ for dimensions.  
7
Fi g u r e 1: Pin Ou t  
www.craneae.com  
Page 3 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
single OUtpUt mOdels COnneCtiOn diagrams - sense and parallel  
12  
11  
10  
9
8
7
1
2
3
4
5
6
Positive Input  
Input Common  
TR1  
INH1  
Sync Out  
Sync In  
MSTR/INH2  
Slave  
Pos. Sense  
+
28V  
Sense Return  
Output Common  
Positive Output  
Inhibit  
+
Sync In  
R
L
REMOTE SENSE CONNECTION  
12  
11  
10  
9
8
7
1
2
3
4
5
6
Positive Input  
Input Common  
TR1  
INH1  
Sync Out  
Sync In  
MSTR/INH2  
Slave  
Pos. Sense  
+
28V  
RA  
Inhibit  
Sense Return  
Output Common  
Positive Output  
+
Sync In  
R
L
OUTPUT VOLTAGE ADJUST CONNECTION  
RA (OHMS)  
VOUT INCREASE  
(VOLT)  
0.1  
3.3–V  
5–V  
12–V 15–V  
120  
240  
360  
480  
600  
70  
25  
50  
20  
40  
0.2  
0.3  
0.4  
0.5  
140  
210  
280  
350  
75  
60  
100  
125  
80  
100  
Fi g u r e 2: Se n S e cO n n e c t i O n S a n D tr i m ta b l e  
12  
11  
10  
9
1
2
3
4
5
6
Positive Input  
Input Common  
TR1  
MSTR/INH2  
Slave  
+
28V  
Pos. Sense  
MASTER  
Inhibit  
INH1  
Sense Return  
Output Common  
Positive Output  
+
8
Sync Out  
Sync In  
7
Sync In  
R
L
CONNECT ONLY WHEN 2 SLAVES ARE USED  
12  
11  
10  
9
1
2
3
4
5
6
Positive Input  
Input Common  
TR1  
MSTR/INH2  
Slave  
Pos. Sense  
SLAVE 1  
INH1  
Sense Return  
Output Common  
Positive Output  
8
Sync Out  
Sync In  
7
1
2
3
4
5
6
12  
11  
10  
9
Positive Input  
Input Common  
TR1  
MSTR/INH2  
Slave  
Pos. Sense  
SLAVE 2  
INH1  
Sense Return  
Output Common  
Positive Output  
8
Sync Out  
Sync In  
7
Fi g u r e 3: Pa r a l l e l cO n n e c t i O n S  
www.craneae.com  
Page 4 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
mOdel nUmbering key  
SMFLHP 28 05 S / K  
Base Model  
R
Input Voltage  
Output Voltage  
Number of Outputs  
(S = single, D = dual)  
Screening  
Radiation Level  
mOdel seleCtiOn  
SMFLHP28  
base model  
/
V
value  
number of outputs  
screening  
out  
Choose one from each of the following rows:  
V
value  
for singles 3R3, 5, 12, 15 for duals: 5, 12, 15  
“R”ꢀ=ꢀdecimalꢀpoint,ꢀꢀ3R3ꢀ=ꢀ3.3VDC  
S (single) or D (dual)  
out  
Number of outputs  
Case option  
standard (case ꢁ, leave blank)  
Screening  
OO* - Space prototype, HO, HP, HR, KR  
*Interpoint model numbers use an “O” in the RHA designator position to indicate the “-” (dash) Radiation Hardness Assurance level  
of MIL-PRF-38534,which is defined as “no RHA”  
www.craneae.com  
Page 5 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Electrical Characteristics: –55°C to +125°C Tc, 28 VDC Vin, 100% load, free run, unless otherwise specified.  
SINꢀLE OꢁTPꢁT MODELS  
SMFLHP283R3S SMFLHP2805S SMFLHP2812S SMFLHP2815S  
MIN TYP MAX MIN TYP MAX MIN TYP MAX MIN TYP MAX  
3.26 3.30 3.34 4.95 5.00 5.05 11.88 12.00 12.12 14.85 15.00 15.15  
unitS  
Parameter  
cOnDitiOnS  
tc = 25°c  
OutPut VOltage  
OutPut current  
OutPut POWer  
VDc  
a
Vin = 19 tO 40 VDc  
Vin = 19 tO 40 VDc  
tc = 25°c  
0
10  
20  
0
16  
53  
25  
40  
50  
20  
0
15  
30  
0
16  
80  
50  
90  
50  
20  
0
7.5  
90  
0
6.67  
100  
95  
0
0
0
0
W
OutPut riPPle  
10 khz - 2 mhz  
19  
30  
85  
30  
45  
mV p-p  
tc = -55°c tO +125°c  
Vin = 19 tO 40 VDc  
nO lOaD tO Full  
45  
0
150  
50  
175  
50  
line regulatiOn  
lOaD regulatiOn  
0
mV  
mV  
VDc  
V
0
0
0
20  
0
20  
inPut VOltage  
cOntinuOuS  
28  
70  
9
40 19  
28  
70  
9
40 19  
28  
40 19  
28  
40  
nO lOaD tO Full  
1, 2  
TRANSIENT  
50 ms  
50  
120  
15  
50  
120  
15  
80  
9
50  
120  
15  
50  
inPut current  
nO lOaD  
80  
120  
15  
mA  
inhibiteD - inh1  
inhibiteD - inh2  
10 khz - 10 mhz  
9
35  
30  
80  
35  
30  
80  
35  
30  
80  
35  
30  
80  
inPut riPPle  
current  
80  
80  
80  
80  
mA p-p  
eFFiciencY  
tc = 25°c  
70  
72  
77  
80  
81  
86  
82  
87  
%
W
lOaD Fault  
tc = 25°c  
ShOrt circuit  
POWer DiSSiPatiOn  
15  
1.5  
22  
10  
15  
1.5  
20  
4
15  
1.5  
20  
4
15  
20  
4
1
1.5  
ms  
recOVerY  
SteP lOaD  
reSPOnSe  
50% - 100% - 50%  
tranSient  
350  
400  
350  
450  
450  
700  
450  
700  
mV pk  
1, 3  
recOVerY  
1.5  
3.0  
1.5  
3.0  
1.5  
3.0  
1.5  
3.0  
ms  
SteP line  
reSPOnSe  
19 - 40 -19 VDc  
250  
400  
250  
400  
250  
800  
250  
800  
mV pk  
1
4
tranSient  
3
recOVerY  
200  
3.5  
300  
10  
200  
3.5  
600  
10  
200  
3.5  
600  
10  
200  
3.5  
600  
10  
µs  
Start-uP  
DelaY  
ms  
1
OVerShOOt  
0
50  
0
25  
0
50  
0
50  
mV pk  
Notes  
1. Gꢆꢄꢈꢄꢁꢉꢃꢃꢅ by ꢅꢃꢊꢀgꢁ, ꢁꢇꢉ ꢉꢃꢊꢉꢃꢅ.  
2. ꢁnit will shut down above approximately 45V but will be undamaged and will restart  
when voltage drops into normal range.  
3. Recovery time is measured from application of the transient to point at which Vout  
is within 1% of final value.  
4. Transition time >10 µs.  
www.craneae.com  
Page 6 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Electrical Characteristics: –55°C to +125°C Tc, 28 VDC Vin, 100% load, free run, unless otherwise specified.  
DꢁAL OꢁTPꢁT MODELS  
SMFLHP2805D SMFLHP2812D SMFLHP2815D  
MIN TYP MAX MIN TYP MAX MIN TYP MAX  
4.95 5.00 5.05 11.88 12.00 12.12 14.85 15.00 15.15  
4.92 5.00 5.08 11.80 12.00 12.18 14.77 15.00 15.23  
unitS  
VDc  
Parameter  
cOnDitiOnS  
OutPut VOltage  
tc = 25°c  
+ V  
Out  
- V  
Out  
2
OutPut current  
Vin = 19 tO 40 VDc  
each OutPut  
0
0
11.2  
16.0  
0
0
5.3  
7.5  
0
0
4.67  
6.67  
a
tOtal  
each OutPut  
tOtal  
2
OutPut POWer  
0
0
56  
80  
0
0
63  
90  
0
0
70  
W
Vin = 19 tO 40 VDc  
100  
OutPut riPPle  
+ V  
25  
25  
150  
150  
50  
50  
175  
175  
50  
50  
225  
225  
Out  
mV p-p  
mV  
10 khz - 2 mhz  
+ V  
- V  
Out  
line regulatiOn  
0
50  
0
50  
0
50  
Out  
V
= 19 tO 40 VDc  
in  
25  
100  
25  
100  
25  
100  
- V  
Out  
lOaD regulatiOn  
nO lOaD tO Full  
+ V  
- V  
0
50  
10  
50  
100  
200  
10  
50  
100  
200  
Out  
mV  
25  
100  
Out  
See nOte 3  
See nOte 4  
cOntinuOuS  
1, 5  
crOSS regulatiOn  
tc = 25°c  
6
8
8
2
4
4
2
4
4
%
7
28  
2
28  
2
28  
inPut VOltage  
nO lOaD tO Full  
19  
0
40 19  
40 19  
40  
50  
VDc  
V
50  
0
50  
0
TRANSIENT  
50 ms  
inPut current  
tc = 25°c  
nO lOaD  
50  
9
120  
14  
50  
9
120  
14  
50  
9
120  
14  
inhibiteD - inh1  
inhibiteD - inh2  
10 khz - 10 mhz  
mA  
35  
80  
35  
80  
35  
80  
inPut riPPle  
current  
30  
80  
80  
30  
86  
80  
30  
87  
80  
mA p-p  
eFFiciencY  
tc = 25°c  
balanceD lOaD  
75  
81  
82  
%
lOaD Fault  
tc = 25°c  
POWer DiSSiPatiOn  
ShOrt circuit  
15  
20  
15  
20  
15  
20  
W
1.5  
4.0  
1.5  
4.0  
1.5  
4.0  
ms  
1, 6  
recOVerY  
SteP lOaD  
reSPOnSe  
50% - 100% - 50% tranSient  
350  
1.5  
450  
3.0  
450  
1.5  
700  
3.0  
450  
1.5  
700  
3.0  
mV pk  
1, 6  
recOVerY  
ms  
± V  
Out  
1, 7  
SteP line  
reSPOnSe  
19 - 40 -19 VDc tranSient  
250  
200  
600  
300  
250  
200  
800  
600  
250  
200  
800  
600  
mV pk  
1
1, 6  
recOVerY  
± V  
µs  
ms  
Out  
Start-uP  
DelaY  
3.5  
0
20  
25  
3.5  
0
20  
50  
3.5  
0
20  
50  
1
mV pk  
OVerShOOt  
Notes  
1. Gꢆꢄꢈꢄꢁꢉꢃꢃꢅ by ꢅꢃꢊꢀgꢁ, ꢁꢇꢉ ꢉꢃꢊꢉꢃꢅ.  
5. ꢁnit will shut down above approximately 45V but will be undamaged and will  
restart when voltage drops into normal range.  
6. Recovery time is measured from application of the transient to point at which  
Vout is within 1% of final value.  
2. ꢁp to 70% of the total output power (current) is available from either output  
provided the opposite output is carrying 30% of the power (current) in use.  
3. Effect on negative Vout from 50%/50% loads to 30%/70% or 70%/30% loads.  
4. Effect on negative Vout from 50%/50% loads to 10% then 50% load on  
negative Vout  
7. Transition time >10 µs.  
www.craneae.com  
Page 7 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Typical Performance Curves: 25°C Tc , 28 VDC Vin, 100% load, free run, unless otherwise specified.  
90  
85  
90  
85  
80  
75  
70  
65  
60  
90  
85  
80  
19V  
19V  
19V  
28V  
28V  
80  
75  
70  
28V  
40V  
75  
70  
65  
60  
40V  
40V  
65  
60  
10  
30  
50  
70  
90  
10  
30  
50  
70  
90 100  
10  
30  
50  
70  
90  
Output (Watts)  
Output Power (Watts)  
Output Power (Watts)  
SMFLHP2805S & SMFLHP2805D  
Efficiency  
SMFLHP2815S & SMFLHP2815D  
Efficiency  
SMFLHP2812S & SMFLHP2812D  
Efficiency  
Fi g u r e 4  
Fi g u r e 6  
Fi g u r e 5  
0.  
100% to 50%  
20.  
Vout  
40.  
60.  
80.  
50% to 100%  
Vin  
100.  
50 µs/div  
19 to 40 V  
1ms/div  
0.1  
1
10  
100  
Frequency (kHz)  
SMFLHP2805S Step Load Response  
SMFLHP Series Audio Rejection  
SMFLHP2805S Step Line Response  
Fi g u r e 8  
Fi g u r e 9  
Fi g u r e 7  
50% to 100%  
Vin  
Vin  
+Vout  
Vout  
–Vout  
100% to 50%  
1ms/div  
No Load  
50 µs/div  
19 to 40 V  
1ms/div  
SMFLHP2815D Step Load Response  
SMFLHP2805S Turn On Response  
SMFLHP2815D Step Line Response  
Fi g u r e 10  
Fi g u r e 11  
Fi g u r e 12  
www.craneae.com  
Page 8 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Typical Performance Curves: 25°C Tc , 28 VDC Vin, 100% load, free run, unless otherwise specified.  
8
19  
6
SMFLHP2805S & 5D  
SMFLHP2805D  
V
IN  
+Vout  
4
2
18  
17  
16  
SMFLHP2812D  
SMFLHP2815S  
0
& 15D  
– 2  
– 4  
SMFLHP2815D  
– 6  
– 8  
–Vout  
SMFLHP2812S & 12D  
1ms/div  
No Load  
30  
40  
50  
60  
70  
30 40 50 60 70 80 90 100  
Output Load (%)  
Output Power (Watts)  
Low Line Dropout  
+Pout 70 to 30 %, –Pout 30 to 70%  
Cross Regulation  
SMFLHP2815D Turn On Response  
Fi g u r e 14  
Fi g u r e 15  
Fi g u r e 13  
700  
600  
500  
400  
300  
200  
125°C  
25°C  
100°C  
100  
0
-55°C  
10  
100  
1000  
10000  
Vin Rise-time (µs)  
SMFLHP2815D Line Transient Response  
vs. Vin Rise-time  
Fi g u r e 16  
www.craneae.com  
Page 9 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈ cꢄꢊꢃꢊ  
28 Volt input – 100 Watt  
TOP VIEW CASE U  
Flanged case, short-leaded  
*Case U does not require designator in Case Option position oꢀ model number.  
Seam Seal  
Angled corner  
0.23 (5.8) Lead Length  
0.128 dia  
(3.25).  
indicates pin one.  
1.505 (38.23) max.  
1.380 (35.05)  
0.040 dia  
(1.02)  
1.250 (31.75)  
1.050 (26.67)  
0.850 (21.59)  
0.650 (16.51)  
0.450 (11.43)  
0.250 (6.35)  
0.120 (3.05)  
0.000  
Case dimensions in inches (mm)  
Tolerance 0.005 (0.13) ꢀor three decimal places  
0.01 (0.3) ꢀor tꢁo decimal places  
unless otherꢁise speciꢀied  
CAUTION  
Heat ꢀrom reꢀloꢁ or ꢁave soldering may damage the device.  
Solder pins individually ꢁith heat application not exceeding 300°C ꢀor 10 seconds per pin  
Materials  
Header Cold Rolled Steel/Nickel/Gold  
Cover Kovar/Nickel  
Pins  
#52 alloy/Nickel/Gold; compression glass seal  
Case U, Rev C, 20060302  
Please reꢀer to the numerical dimensions ꢀor accuracy. All inꢀormation is believed to be accurate,  
but no responsibility is assumed ꢀor errors or omissions. Interpoint reserves the right to make  
changes in products or speciꢀications ꢁithout notice.  
Copyright © 1999-2006 Interpoint Corp. All rights reserved.  
Fi g u r e 16: ca S e u  
www.craneae.com  
Page 10 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Cl a s s H a n d K, MIl-PRF-38534 El E M E n t Ev a l u a t I o n  
COmpOnent-level test  
perfOrmed  
spaCe prOtOtype (O)  
Class h  
Qml  
Class k  
Qml  
1
nOn-Qml  
2
3
2
3
2
3
M/s  
P
M/s  
P
M/s  
P
Element Electrical  
Element Visual  
yes  
no  
no  
no  
yes  
yes  
yes  
yes  
yes  
yes  
yes  
yes  
Internal Visual  
no  
no  
no  
no  
no  
no  
no  
N/A  
no  
no  
no  
no  
no  
N/A  
no  
yes  
no  
N/A  
no  
yes  
yes  
yes  
yes  
yes  
yes  
yes  
N/A  
N/A  
yes  
yes  
yes  
no  
N/A  
yes  
yes  
N/A  
N/A  
N/A  
N/A  
yes  
yes  
yes  
yes  
N/A  
yes  
Temperature Cycling  
Constant Acceleration  
Interim Electrical  
Burn-in  
no  
no  
no  
N/A  
N/A  
N/A  
N/A  
no  
no  
N/A  
N/A  
N/A  
N/A  
no  
no  
Post Burn-in Electrical  
Steady State Life  
Voltage Conditioning Aging  
Visual Inspection  
Final Electrical  
no  
no  
N/A  
N/A  
yes  
yes  
no  
no  
no  
no  
yes  
yes  
N/A  
yes  
4
Wire Bond Evaluation  
no  
SEM  
N/A  
no  
SLAM™/C-SAM:  
no  
Input capacitors only  
(Add’l test, not req. by H or K)  
Notes:  
1. Non-QML products do not meet all of the requirements of MIL-PRF-38534.  
2.ꢀM/Sꢀ=ꢀActiveꢀcomponentsꢀ(MicrocircuitꢀandꢀSemiconductorꢀDie)  
3.ꢀPꢀ=ꢀPassiveꢀcomponentsꢀꢀ  
4. Not applicable to EMI filters that have no wirebonds.  
Definitions:  
Element Evaluation: Component testing/screening per MIL-STD-883 as determined by MIL-PRF-38534  
SEM: Scanning Electron Microscopy  
SLAM™: Scanning Laser Acoustic Microscopy  
C-SAM: C - Mode Scanning Acoustic Microscopy  
www.craneae.com  
Page 11 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Cl a s s H a n d K, MIl-PRF-38534 En v I R o n M E n t a l sC R E E n I n g  
end item-level test  
perfOrmed  
spaCe prOtOtype (O)  
Class h  
Qml  
Class k  
Qml  
1
nOn-Qml  
2
Non-destruct bond pull  
Method 2023  
no  
yes  
yes  
yes  
Pre-cap Inspection  
Method 2017, 2032  
yes  
yes  
Temperature Cycle (10 times)  
Method 1010, Cond. C, -65°C to 150°C, ambient  
yes  
yes  
yes  
yes  
yes  
yes  
Constant Acceleration  
Method 2001, 3000 g  
PIND Test  
Method 2020, Cond. A  
2
no  
yes  
yes  
yes  
Pre burn-in test  
yes  
yes  
Burn-in  
Method 1015, 125°C case, typical  
96 hours  
160 hours  
yes  
no  
no  
no  
yes  
no  
no  
no  
yes  
2 x 160 hours (includes mid-BI test)  
Final Electrical Test MIL-PRF-38534  
Group A, Subgroups 1 through 6  
-55°C, +25°C, +125°C case  
yes  
N/A  
N/A  
yes  
N/A  
N/A  
yes  
N/A  
Radiography  
Method 2012  
Post Radiography Electrical Test  
Room temperature  
2
yes  
Hermeticity Test  
Fine Leak, Method 1014, Cond. A  
Gross Leak, Method 1014, Cond. C  
yes  
yes  
yes  
yes  
yes  
yes  
Final visual inspection  
Method 2009  
yes  
yes  
yes  
Test methods are referenced to MIL-STD-883 as determined by MIL-PRF-38534.  
Notes:  
1. Space Prototype (O), non-QML products, do not meet all of the requirements of MIL-PRF-38534.  
2. Not required by DSCC but performed to assure product quality.  
www.craneae.com  
Page 12 of 13  
Rev H - 20071221  
Crane Aerospace & Electronics Power Solutions  
smFlHp sꢀꢁgꢂꢃ ꢄꢁꢅ dꢆꢄꢂ dc/dc cꢇꢁvꢃꢈꢉꢃꢈꢊ  
28 Volt input – 100 Watt  
Cl a s s H a n d K, MIl-PRF-38534 Ra d I a t I o n as s u R a n C E  
EnvIRonMEntal sCREEnIng lEvEls  
sPaCE  
PRototYPE (o)  
Class H  
QMl  
Class K  
QMl  
RadIatIon HaRdnEss  
assuRanCE lEvEls  
2
n o n -QMl  
1
O : Standard, no radiation guarantee  
OO  
N/A  
N/A  
HO  
N/A  
N/A  
p: Radiation tolerant–Tested lots up to 30 K  
Rads (Si) total dose  
SEU guarantee up to 40 MeV  
3
HP  
r: Radiation tolerant–Tested lots up to 100 K  
Rads (Si) total dose  
3
3
HR  
KR  
SEU guarantee up to 40 MeV  
Notes:  
1. Interpoint model numbers use an “O” in the RHA designator position to indicate the “-” (dash)  
Radiation Hardness Assurance level of MIL-PRF-38534, which is defined as “no RHA”.  
2. Space Prototype (O), non-QML, products do not meet all of the requirements of MIL-PRF-38534.  
3. Redmond site, Interpoint, has a Radiation Hardness assurance plan on file with DSCC. Our SMD products with RHA “P" and "R" code  
meet DSCC requirements.  
SMFLHP Single and Dual, Rev H - 20071221. This revision supercedes all previous releases. All technical information is believed to be accurate,  
but no responsibility is assumed for errors or omissions. Interpoint reserves the right to make changes in products or specifications without notice.  
SMFLHP Series is a trademark of Interpoint. Copyright © 1999 - 2007 Interpoint Corporation. All rights reserved. www.craneae.com  
Page 13 of 13  

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