JASA Standards Handbook Version 2.0

30 October 1997


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CHAPTER 8.   PHYSICAL SERVICES

8. PHYSICAL SERVICES
8.1 Introduction
8.2 Mandates
8.2.1 Chassis
8.2.2 Backplanes
8.2.3 Circuit Cards
8.2.4 Power Quality
8.2.5 Environmental Standards
8.2.6 TEMPEST
8.2.7 EMI/EMC
8.3 Emerging Technologies
8.3.1 Backplanes
8.3.2 Circuit Cards


8.   PHYSICAL SERVICES

8.1   INTRODUCTION

     Physical Services identify the standards necessary to integrate SIGINT sensors into an airborne environment. Physical services address the areas of size, weight, and power (SWAP) as well as unique airborne environmental conditions. These services include chassis, backplanes, circuit cards, power quality, and Electromagnetic Compatibility (EMC).

     The standards specified in this chapter are either platform independent, or they are identified as being applicable to Category I (benign), II (harsh), or III (ground) environments.

     Category I is a relatively benign airborne environment, where equipment SWAP are concerns but not major issues. Examples of Category I are Rivet Joint (RJ) and Airborne Reconnaissance Low (ARL).

     Category II is a harsh airborne environment, where equipment SWAP are major issues. Examples of Category II are Air Force Special and Unmanned Aerial Vehicles (UAV).

     Category III is a non-airborne environment, where equipment SWAP are not necessarily major issues. Examples of Category III are Contingency Airborne Reconnaissance System (CARS) and Consolidated Remote Operations Facility, Airborne (CROFA).

8.2   MANDATES

     8.2.1   Chassis

     Category I and Category III equipment chassis shall (Category II equipment chassis should) comply with the following:

  • EIA-310C 19" Rack Standard or

  • ARINC 404 Air Transport Requirements Standard (ATR)

  • 8.2.2   Backplanes

         Backplanes with primarily RF boards shall use:

  • IEEE STD 1155-1992 (VXI-C)

  •      Backplanes with primarily digital boards shall use:

  • ANSI/VITA 1-1994 (VME64-B)

  •      8.2.3   Circuit Cards

         Circuit Card Assemblies (CCA) shall be either:

  • ANSI/VITA 1-1994 (VME64-B)

  • or

  • IEEE STD 1155-1992 (VXI-C)

  •      Systems requiring conduction cooling shall comply with the following:

  • IEEE 1101.2

  •      8.2.4   Power Quality

         Category I and II, shall comply with the following:

  • MIL-STD-704E

  •      It is preferable for Category III to also comply, as some "ground" systems are powered by generators, or located on moving vehicles (air, land, and sea) and may be subject to dirty power.

         8.2.5   Environmental Standards

         Category I hardware shall comply with the following:

  • Radio Technical Commission for Aeronautics, RTCA DO-160C

  •      8.2.6   TEMPEST

         For equipment that may tie directly to a transmitter or Communications Security (COMSEC) device or that may impinge on the red-black interface, TEMPEST requirements and applicability must be considered. The following shall apply:

  • NSTISSP 300, National Policy on Control of Compromising Emanations

  • NSTISSI 7001, NONSTOP Countermeasures


  • 1 VME64-B equates to a 6U-160 card size.

  • NSTISSAM TEMPEST/2-95, Guidelines for Facility Design and Red/Black Installation

  • NACSEM 5112, NONSTOP Evaluation Techniques

  •      8.2.7   EMI/EMC

         Commercial items shall comply with the following:

  • FCC Title 47, part 15 (Radio Frequency Devices) rules

  •      To minimize interference, electronic equipment shall comply with the following:

  • MIL-STD-461D-EMI Compatibility Standard, Electromagnetic Emission and Susceptibility Requirements for the Control of Electromagnetic Interference as shown in Table 8-1 and tested in accordance with MIL STD 462D

  • 8.3   EMERGING TECHNOLOGIES

         8.3.1   Backplanes

         8.3.2   Circuit Cards



    2 Some platforms may have more stringent EMI/EMC requirements/specification that need to be adhered to for that platform.


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