MIL-STD-1760E-2007_Aircraft_Store_Electrical_Interconnection_System.PDF

MIL-STD-1760

GJB1188A-1999

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METRIC

MIL-STD-1760E

24 October 2007

________________

SUPERSEDING

MIL-STD-1760D

1 August 2003

DEPARTMENT OF DEFENSE

INTERFACE STANDARD

AIRCRAFT/STORE ELECTRICAL

INTERCONNECTION SYSTEM

AMSC: N/A AREA: SESS

DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.

MIL-STD-1760E

FOREWORD

1. This standard is approved for use by all Departments and Agencies of the Department of Defense.

2. Prior to this standard, an aircraft and the stores which it carried were typically

developed

independently of each other

or were developed exclusively for each other.

This usually resulted in unique

aircraft/store electrical interconnection requirements, the general proliferation of overall store interface

designs,

low levels of interoperability, and costly airc

raft modifications to achieve required store utilization

flexibility. Trends in store technology toward more

complex

store functions which require increasing

amounts of avionics data and control information

from aircraft

systems were predicted to lead to

insurmountable aircraft/store interfacing problems.

The goal is to develop aircraft that are compatible

with a wide variety of stores and stores that are

compatible with a wide variety of

aircraft. Th

is standard supports this goal by defining a standard

electrical (and fiber optic) interconnection system for aircraft

and

stores. This interconnection system is

based on use of a standard connector, a standard signal set and a standard serial digital data interface

for control, monitor, and release of stores. Application of this standard to new and existing aircraft and

new stores will significantly reduce and stabilize the number and variety of

signals required

aircraft/store

interfaces, minimize the impact of new stores on future stor

es management systems, and

increase store interoperability among the services, within NATO, and with other allies.

4. Revision E does not change the fundamental MI

L-STD-1760 interface. It includes newly defined

requirements

for a Fibre Channel interface, splits

APPENDIX B

into two parts, and makes other minor

changes and corrections.

5. Changes between Revision D and Revision E are not

marked in this document, but note references

are added in the text, referring to notes in APPENDIX E

that explain the significant technical changes.

6. Some requirements in MIL-STD-1760 are stated by invoking other documents, including MIL-STD-

1553 and MIL-DTL-38999. If tiering of requirements is lim

ited to one level on a particular contract, it may

be necessary to include references to these second tier documents in the contractual specification.

7. The following areas are limitations of this standard:

Requirements for mechanical, aerodynamic, logistic, and

operational compatibility are not

covered.

Since factors such as size, shape, loads, clearances, and

functional limitations are not specified,

full operability of stores on aircraft cannot be assured.

c. Signals for emergency jettison of stores are not specified. However, this does not preclude the

use of the signals in this standard if they are compatible with the requirements for emergency jettison.

This standard does not attempt to establish the EMI/EMC requirements on the aircraft or

store,

although it does define an interface that is generally capable of meeting these requirements.

Comments, suggestions, or questions on this document should be addressed to:

ASC/ENOI,

2530

Loop Road West, Wright-Patterson AFB, Ohio 45433-7101 or email

Engineering.Standards@wpafb.af.mil. Since contact information can change, you may want to verify the

currency of this address information using the ASSIST Online database at http://assist.daps.dla.mil

MIL-STD-1760E

CONTENTS

PARAGRAPH PAGE

iii

[Note 1]

SCOPE....................................................................................................................................1

1.1 Scope. ..................................................................................................................................... 1

1.2 Purpose. .................................................................................................................................. 1

1.3 Application............................................................................................................................... 1

2 APPLICABLE DOCUMENTS ..................................................................................................2

2.1 General.................................................................................................................................... 2

2.2 Government documents..........................................................................................................2

2.2.1 Specifications, standards, and handbooks. ............................................................................2

2.2.2 Other government documents, drawings, and publications.................................................... 2

2.3 Non-Government publications................................................................................................. 3

2.4 Order of precedence. .............................................................................................................. 3

3 DEFINITIONS.......................................................................................................................... 4

3.1 Definitions................................................................................................................................4

3.1.1 Aircraft. .................................................................................................................................... 4

3.1.2 Aircraft/store Electrical Interconnection System (AEIS).......................................................... 4

3.1.3 Electrical interface types. ........................................................................................................ 4

3.1.3.1 Aircraft Station Interface (ASI)................................................................................................. 4

3.1.3.2 Carriage Store Interface (CSI). ...............................................................................................4

3.1.3.3 Carriage Store Station Interface (CSSI).................................................................................. 4

3.1.3.4 Mission Store Interface (MSI)..................................................................................................4

3.1.3.5 Routing Network Aircraft Subsystem Port (RNASP)............................................................... 4

3.1.4 Provisions................................................................................................................................ 4

3.1.5 Store........................................................................................................................................ 5

3.1.5.1 Carriage stores........................................................................................................................ 5

3.1.5.2 Mission stores. ........................................................................................................................ 5

3.1.5.3 Dispensers. ............................................................................................................................. 5

3.1.6 Stores management system. .................................................................................................. 5

3.1.7 Suspension and release equipment (S&RE). .........................................................................5

3.1.8 Random noise. ........................................................................................................................ 5

3.1.9 Periodic noise.......................................................................................................................... 5

3.1.10 Impulse noise. ......................................................................................................................... 5

3.1.11 Stimulated noise...................................................................................................................... 5

3.1.12 Common mode noise. ............................................................................................................. 5

3.1.13 Latency.................................................................................................................................... 6

3.1.14 Delay. ...................................................................................................................................... 6

3.1.15 Power interruption. .................................................................................................................. 6

3.1.16 Safety Critical. [Note 4]........................................................................................................... 6

3.1.17 DC Offset................................................................................................................................. 6

3.1.18 Fibre Channel.......................................................................................................................... 6

3.2 Acronyms and abbreviations................................................................................................... 6

4 GENERAL REQUIREMENTS .................................................................................................8

4.1 Aircraft/store configurations. ................................................................................................... 8

4.2 Interface classes. [Note 3]...................................................................................................... 8

4.3 Primary interface signal set..................................................................................................... 8

4.3.1 High bandwidth (HB) interfaces. ............................................................................................. 8

4.3.1.1 Type A signal requirements. .................................................................................................11

4.3.1.2 Type B signal requirements. .................................................................................................11

4.3.1.3 Signal assignment................................................................................................................. 11

4.3.2 Data bus interfaces. ..............................................................................................................12

4.3.2.1 MIL-STD-1553 data bus interface. [Note 5] ......................................................................... 12

MIL-STD-1760E

CONTENTS

PARAGRAPH PAGE

4.3.2.2

Fibre Channel interface. [Note 3] ......................................................................................... 12

4.3.3 Low bandwidth (LB) interface................................................................................................ 12

4.3.3.1 LB signal requirements.......................................................................................................... 12

4.3.3.2 Signal assignment................................................................................................................. 12

4.3.4 Release consent interface.....................................................................................................14

4.3.5 Primary interlock interface..................................................................................................... 14

4.3.6 Address interface. .................................................................................................................15

4.3.7 Primary structure ground....................................................................................................... 15

4.3.8 Primary power. ...................................................................................................................... 15

4.3.9 Fiber optic (FO) interfaces. ................................................................................................... 15

4.4 Auxiliary power interface signal set....................................................................................... 15

4.4.1 Auxiliary power. ..................................................................................................................... 15

4.4.2 Auxiliary interlock interface....................................................................................................15

4.4.3 Auxiliary structure ground......................................................................................................16

4.5 Interface connectors.............................................................................................................. 16

5 DETAILED REQUIREMENTS...............................................................................................17

5.1 Aircraft requirements............................................................................................................. 17

5.1.1 Aircraft HB interfaces. ...........................................................................................................17

5.1.1.1 Minimum transfer capacity. ................................................................................................... 17

5.1.1.2 Type A signal path requirements. .........................................................................................17

5.1.1.2.1 Return loss. ........................................................................................................................... 17

5.1.1.2.2 Transient response................................................................................................................ 17

5.1.1.2.3 Insertion gain.........................................................................................................................17

5.1.1.2.4 Representative pulse delay................................................................................................... 17

5.1.1.2.5 Equalization........................................................................................................................... 17

5.1.1.2.6 Dynamic range. .....................................................................................................................18

5.1.1.2.7 Signal path dc offset.............................................................................................................. 18

5.1.1.2.8 Noise requirements. ..............................................................................................................18

5.1.1.2.8.1 Random noise. ...................................................................................................................... 18

5.1.1.2.8.2 Periodic noise........................................................................................................................ 18

5.1.1.2.8.3 Impulse noise. .......................................................................................................................18

5.1.1.2.8.4 Stimulated noise.................................................................................................................... 18

5.1.1.2.8.5 Common mode noise. ........................................................................................................... 18

5.1.1.3 Type B signal path requirements. .........................................................................................18

5.1.1.4 Ground reference. ................................................................................................................. 18

5.1.2 Aircraft MIL-STD-1553 data bus interface. ........................................................................... 19

5.1.2.1 Functional characteristics...................................................................................................... 19

5.1.2.2 Electrical characteristics........................................................................................................ 19

5.1.2.2.1 Output characteristics............................................................................................................ 19

5.1.2.2.2 Input characteristics. ............................................................................................................. 19

5.1.2.2.3 Shield grounding. ..................................................................................................................19

5.1.3 Aircraft LB interface............................................................................................................... 27

5.1.3.1 Minimum transfer capacity. ................................................................................................... 27

5.1.3.2 Input/output impedance.........................................................................................................27

5.1.3.3 Insertion gain.........................................................................................................................27

5.1.3.4 Equalization requirements..................................................................................................... 27

5.1.3.5 Signal path dc offset.............................................................................................................. 28

5.1.3.6 Noise. .................................................................................................................................... 28

5.1.3.6.1 Periodic and random noise. ..................................................................................................28

5.1.3.6.2 Impulse noise. ....................................................................................................................... 28

5.1.3.6.3 Stimulated noise.................................................................................................................... 28

5.1.3.6.4 Common mode noise. ........................................................................................................... 29

5.1.3.7 Ground reference. ................................................................................................................. 29

MIL-STD-1760E

CONTENTS

PARAGRAPH PAGE

5.1.4

Aircraft release consent interface.......................................................................................... 29

5.1.4.1 Voltage level.......................................................................................................................... 30

5.1.4.2 Current level. ......................................................................................................................... 30

5.1.4.3 Stabilization time. .................................................................................................................. 30

5.1.4.4 Enable lead time.................................................................................................................... 30

5.1.4.5 Inhibit delay. .......................................................................................................................... 30

5.1.4.6 Ground reference. ................................................................................................................. 30

5.1.4.7 Duration of application to mission store. [Note 9] ................................................................30

5.1.5 Aircraft interlock interface...................................................................................................... 31

5.1.6 Aircraft address interface. ..................................................................................................... 31

5.1.6.1 Address assignment.............................................................................................................. 31

5.1.6.2 Address signal....................................................................................................................... 32

5.1.6.3 Logic thresholds. ................................................................................................................... 32

5.1.6.4 Response characteristics...................................................................................................... 32

5.1.6.5 Address isolation................................................................................................................... 32

5.1.7 Aircraft structure ground........................................................................................................ 33

5.1.8 Aircraft 28 V dc power interface. ...........................................................................................33

5.1.8.1 Independent control............................................................................................................... 33

5.1.8.2 Voltage level.......................................................................................................................... 33

5.1.8.3 Current capacity. ................................................................................................................... 33

5.1.8.3.1 Primary signal set..................................................................................................................33

5.1.8.3.2 Auxiliary power signal set...................................................................................................... 33

5.1.8.3.3 Simultaneous current. ...........................................................................................................33

5.1.8.4 Overcurrent protection........................................................................................................... 33

5.1.8.5 Off-state leakage current....................................................................................................... 33

5.1.8.6 Stabilization time. .................................................................................................................. 36

5.1.8.7 Ground reference. ................................................................................................................. 36

5.1.8.8 Power application.................................................................................................................. 36

5.1.9 Aircraft 115/200 V 400 Hz ac power interface. .....................................................................36

5.1.9.1 Independent control and dead facing.................................................................................... 37

5.1.9.2 Voltage level.......................................................................................................................... 37

5.1.9.3 Current capacity. ................................................................................................................... 37

5.1.9.3.1 Primary signal set..................................................................................................................37

5.1.9.3.2 Auxiliary power signal set...................................................................................................... 37

5.1.9.3.3 Simultaneous current. ...........................................................................................................37

5.1.9.4 Overcurrent protection........................................................................................................... 37

5.1.9.5 Off-state leakage current....................................................................................................... 37

5.1.9.6 Stabilization time. .................................................................................................................. 37

5.1.9.7 Phase rotation. ...................................................................................................................... 37

5.1.9.8 Load power factor.................................................................................................................. 38

5.1.9.9 Phase power unbalance........................................................................................................38

5.1.9.10 Ground reference. ................................................................................................................. 38

5.1.9.11 Power application.................................................................................................................. 38

5.1.10 Aircraft 270 V dc power interface.......................................................................................... 38

5.1.10.1 Independent control and dead facing.................................................................................... 38

5.1.10.2 Voltage level.......................................................................................................................... 39

5.1.10.3 Current capacity. ................................................................................................................... 39

5.1.10.3.1 Primary signal set..................................................................................................................39

5.1.10.3.2 Auxiliary power signal set...................................................................................................... 39

5.1.10.3.3 Simultaneous current. ...........................................................................................................39

5.1.10.4 Overcurrent protection........................................................................................................... 39

5.1.10.5 Off-state leakage current....................................................................................................... 39

5.1.10.6 Stabilization time. .................................................................................................................. 39

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