ARIA Aircraft

61-0326
    4950th Call AGAR 21              "Snoopy"
61-0327
    4950th Call AGAR 22
61-0328

    4950th Call AGAR 23
Crashed 6 May 1981. A living Memorial is dedicated to the crew at the WPAFB Museum in Dayton Ohio USA.

61-0329
   
4950th Call AGAR 24
61-0330

     4950th Call AGAR 25
         "Windjammer"
60-0372
60-0374
     4950th Call AGAR 27
           "Bird of Prey"
The Last Remaining       EC-135E ARIA Aircraft in Existence. Housed at the WPAFB Museum in Dayton Ohio USA. One of the original eight Apollo Range Instrumentation Aircraft.

60-0375
 
Transferred to the ARGUS Program.
81-0891

Officially performed the last ARIA mission. Transferred to the Joint Stars Program in 2001.
81-0892
          
"The Beast"
81-0893

Specially modified for the CMMCA Program.
More . . .
81-0894
Transferred to the Joint Stars Program in 2001.
81-0895

Specially modified for the CMMCA Program.
  
 
More . . .
81-0896
            
"Pegasus"
Modified for use as a test bed for SMILS/Optics Program

TRIA Aircraft
62-4128
4950th Call AGAR 06
62-4133
4950th Call AGAR 07

 

 

ARIA Missions
Patrick AFB
1968-1975

Apollo
Chevaline
Hawkeye
Helios
IMP
IntelSat
Lunar Sounder
Mariner
Minuteman III
Nato III
NOAA
Pioneer
SatCom
Skylab
Skynet
SMS
Viking
Westar

WPAFB 1976-1994Advanced Cruise Missile
Air Launched Cruise
Airborne Bistatic Radar
AMRAAM
B-1B
CCRES
Chevaline
COBE
Delta II
FLTSATCOM
Galileo Jupiter
HEAO
LandSat
Magellan Venus Mapper
Mars Observer
Navstar
Peacekeeper
Pershing
Pioneer Venus
Polaris
Poseidon
RCS Satcom
SAMPEX
SeaSat
SDI
STS
TIROS
Titan
Tomahawk
Trident
Voyager
X-Ray Time Explorer

Edwards AFB 1995-2001
FAST
Leonid
Solar and Heliosperic
Titan IV
X-Ray Time Explorer

 

 

 

   

 

 

 

             

 

          

 

The Advanced Range Instrumentation Aircraft History  and ARIA 328 Memorial Web Site
 
Data Separation Console

ARIA's new data separation console (DSC) is a dual redundant PC based (running NT 4.0) system capable of processing, for display and retransmission, multiple 10 Mbps channels. The onboard Ethernet network also allows for integration of other control and display systems, throughout the aircraft, with the new DSC.

Pre- and post-detection processing of the received signals is accomplished in the data separation subsystem. This subsystem is specifically designed to process frequency modulation (FM), pulse-code modulation / bi-phase shift key (PCM/BPSK), PCM/FM, and/or PCM video signals for recording, real-time retransmission, and/or real-time strip out for analysis and mark event reporting.

PCM Decommutator

Two PCM decommutators can be used in PCM data processing or checkout. The decommutator performs the following functions:

  • Frame synchronization, including word-length and frame-length selection
  • 33-bit parallel-binary multiplex output
  • Programmable 10-bit parallel-binary display
  • Analog-display meter
  • 10-bit digital-to-analog conversion
  • Recycle subframe synchronization, including subframe-length selection
  • Identification-type subframe synchronization, including subframe-length selection
  • Binary to binary coded decimal conversion
  • Three-digit decimal display

Bit Synchronizer

The data separation system contains two bit synchronizers, either EMR 720 or Aydin Monitor 335A. Special configurations add additional bit syncs. The bit synchronizer accepts serial PCM data in the presence of noise and other perturbations and generates reconstructed coherent PCM data and timing signals.

Analog Display

The analog display utilizes parallel data from the decommutator to provide the operator with visual analog readouts of two selected events, using 8-bit digital to analog converters. It also provides two corresponding rear panel analog outputs to interface with a visicorder.

Modular Interface Unit (MIU)

The MIU is a microprocessor controlled interface which coordinates and controls inputs from and outputs to the processor, INS, decommutators 1 and 2, thermal printer, and tabletop terminal. It is hard wired to accept a particular group of modular circuit boards, but also serves as a platform for special mission related circuits. The interior of the MIU is divided into 18 modular increments, each capable of holding one 4.2 x 5.0-inch circuit board. Due to this modular design, functional capabilities can easily be added or deleted as mission requirements change. (For special functions implemented by the MIU, see Appendix E.) Capabilities of the MIU also include IRIG time input and limited data processing capabilities to augment the telemetry data processor (TDP). The MIU can process mark event data from either digital or analog data streams and provide a hard copy of time-of-occurrence.

Processor

The processor is a militarized, airborne use computer which uses a 16-bit, bit-slice implementation Micro Module CPU with programmable real-time clock, floating point, and memory allocation and protection. The operating system supports high level languages such as Ada, FORTRAN, and CMS-2; however, all software is presently written in assembly language as stand-alone programs to maximize throughput. The ground system which is used for software development is set up to interface to a Cypher magnetic tape, a Centronix parallel printer, and two 8-inch floppy disk drives.

Disk Drive

The disk drive is an 8-inch floppy type built into the processor chassis. Its primary purpose is to program the processor unit.

Thermal Printer

The printer is a high-speed device which prints graphic and alphanumeric characters on 4.25-inch wide roll paper. Its main function is to print a hard copy of selected data parameters from the processor or TDP, such as missile position and range.

FM Subcarrier Discriminator Assembly

The FM discriminator assembly is a bank of 18 individual discriminator modules which can be configured as any combination of available IRIG proportional bandwidth subcarrier channels. Its purpose is to extract subcarrier channels from an FM multiplex and detect any data on these channels. Signals may be routed to each discriminator individually or to all simultaneously.

VCO/Mixer Assembly

The voltage controlled oscillator (VCO)/mixer assembly is a bank of modules consisting of seven dual channel VCO's, a calibrator, and three summing amplifiers. Its purpose is to modulate low frequency data onto FM subcarriers to create a multiplex for recording or retransmission.

Dual Channel Variable Filter

The variable filter is a unit containing two independent solid state active filters which can operate in either low-pass or high-pass modes. By connecting the filters in series or parallel, the unit can function as a low- or high-pass filter with a sharp rolloff, or a bandpass or band-stop filter.

Visicorder

The visicorder provides visual traces of input data on moving photosensitive paper through the use of a fiber optic cathode ray tube. The visicorder can be used to physically evaluate or time correlate analog phenomena in a data stream.

 

 

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flyARIA.com Web Site Copyright © 2001-2008 Randy L. Losey
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