Aeronautical Systems Center, ASC/WMAK, 102 West D Avenue, Suite 300, Eglin AFB, FL 32542-6808

15 -- SUB SCALE AERIAL TARGET POC Capt Jim Reynods, Program Manager, 850-882-9307, Ext 5123; Mr. Andrew Jacobs, Contract Specialist, 850-882-9307, Ext 5096 MODIFICATION: This is a modification to the sources sought synopsis for Subscale Aerial Targets published on 10 April 1998. Delete the following section: "b. Performance Parameters. (1) Payloads: Specific payloads which the target must be compatible with include, but are not limited to, the Midi-Pod with ULQ-21 ECM components, the APC-4 and AZC-1 IR Augmentation pods, and the ALE-44 chaff/flare dispensers. (2) Target Flight Performance: The target must meet or exceed all of the following flight performance requirements when flying with the baseline operational payload configuration. The baseline operational payload configuration is defined as two 150 lb. Midi pods with ULQ-21 ECM components and two ALE-44 chaff/flare dispensers. The target shall operate within an altitude range of 1000 ft AGL to 45,000 ft MSL. The target shall have a speed range of 250 knots to .85 Mach in level flight. The target shall be capable of performing a 6G, constant speed, 360 degree turn at or below 20,000 ft MSL while losing no more than 1500 ft of altitude." Replace with the following section: "b. Performance Parameters. (1) Payloads: The target shall have wingtip payload stations rated to 100 lbs. each and underwing hardpoints rated to 150 lbs. each. Specific payloads which the target must be compatible with include, but are not limited to, the Midi-Pod with ULQ-21 ECM components, IR Augmentation pods, and the ALE-44 chaff/flare dispensers. (2) Target Flight Performance: The target must meet or exceed all of the following flight performance requirements when flying with the baseline operational payload configuration. The baseline operational payload configuration is defined as two 100 lb. Midi pods with ULQ-21 ECM components and two ALE-44 chaff/flare dispensers. The target shall operate within an altitude range of 1000 ft AGL to 45,000 ft MSL. The target shall have a speed range of 250 knots to .85 Mach in level flight. The target shall be capable of performing a 6G, constant speed, 360 degree turn at or below 20,000 ft MSL while losing no more than 1500 ft of altitude." At the end of the initial CBD, after the words -- "Collect calls will not be accepted," add the following sentence: "A summary of questions and responses will be posted on the internet at www.asc.eglin.af.mil/wma." As noted previously, the statement of capability(SOC) is due not later than 8 May 1998. (0111)

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