Selected by Boeing for the 767 Global Tanker Transport Aircraft

Software upgrade to the TCAS 2000 or TēCAST

Enhanced surveillance volume

Supports clustering of up to 50 aircraft

Designed to comply with ATC guidelines

Higher resolution ranges for close-in operations

Complete surveillance solution: TCAS, TAWS and Mode S/IFF products

Unrestricted formation/rendezvous capabilities within civil airspace No platform, clustering or altitude restrictions)
Brochure
 
Military Enhanced TCAS The Next Generation

The Flexible Solution


ACSS has developed a military-specific application from our commercial surveillance system that addresses unique requirements of the military. This set of technologies is known as Military Airborne Surveillance System (MASS™) and is based on commercial Automatic Dependent Surveillance-Broadcast (ADS-B) technology. The ACSS Cooperative Member functionality, a subset of MASS, is a software change to the TCAS 2000 or T²CAS™ computer and the Mode S/IFF Transponder that provides a system capable of supporting unique military flight requirements such as formation flight and rendezvous operations in commercial airspace.

The use of ADS-B and adaptive power level interrogation techniques will prevent interference with the civil ATC environment. The system will include cooperative member identification using Flight ID and Mode S address, unique cockpit display characteristics for cooperative members, and the ability to select an aircraft for display of specific aircraft data.

In addition to standard TCAS modes, the MASS product provides military operational modes that support operation in cooperative flight situations such as large formation or rendezvous operations. When Cooperative Flight Mode is not selected, the system will perform normally as a TCAS/ACAS II collision avoidance system. The MASS product is easily upgradeable to TēCAS™ by adding the innovative Thales Avionics Ground Collision Avoidance Module TAWS system to the TCAS 2000 LRU.

 
Technical Specifications
TCAS R/T  
Physical Dimensions (W x H x D) 4.9 x 7.6 x 15.2 in.
Weight 14.7 lbs.
Power 28 Vdc or 115 Vac
Environmental Temperature (Operating) -55 to +70° C
Altitude 55,000 Ft.
Cooling No Cooling Required
Environment ARINC DO-160C
Shock, Vibration  
EMI                        

MIL810
MIL461

   
XS950SI Mode S/IFF Transponder  
Physical Dimensions (W x H x D) 4.9 x 7.6 x 15.2 in.
Weight 11.5 lbs.
Power 28 Vdc or 115 Vac
Environmental Temperature (Operating) -55° to +70° C
Altitude 55,000 Ft.
Cooling Per ARNIC 600
Environment ARINC DO-160D
Shock, Vibration
EMI
   
Optional CDTI Display  
Physical Bezel Dimensions 4.815 in. x 6.25 in.
Image Size 5.1 in. (W) x 3.8 in. (H), 6.3 in. diag.
Case Size ARINC 708A
Weight 6.5 lbs.
   
Interfaces  
TCAS ARINC 429/735 & 735A
TAWS ARINC 762/453
FMS ARINC 702 (growth)
DME ARINC 568 (growth)
INS ARINC 561 (growth)
Weather Radar ARINC 708A, Collins WRX-700X,
Honeywell RDR-4A/RDR-4B
55,000 Ft.