Attachment 03 MQM-186 Aerial Target Demonstrated Performance.pdf

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Attached to
U. S. Army's Air Defense Artillery Targets (ADA-T) Federal contract opportunity
Solicitation number
W900KK21R0029
Issued by
Department of the Army Materiel Command Contracting Command Orlando Contracting Center

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This document contains a sources sought notice and performance specifications for aerial target systems to support Army training requirements. The U.S. Army is seeking sources to produce MQM-170, MQM-171, and MQM-186 aerial targets in accordance with the specifications provided. Interested vendors must demonstrate the ability to meet all threshold performance requirements for airspeed, endurance, payload capacity, altitude, range, and other criteria. Responses are requested by March 23, 2021 to inform the development of a follow-on indefinite delivery/indefinite quantity contract for aerial target production and services. The anticipated award date for the IDIQ is the first quarter of fiscal year 2022. The Army intends to set aside this requirement fully for small businesses under NAICS code 336411.

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MQM-186 A/B

Group 2 Aerial Target

Demonstrated Performance

22 January 2021

MQM-186 A/B Group 2, Aerial Target Performance Requirements

Table 1: MQM-186, Requirements and Demonstrated Performance

Description Threshold Requirement

Objective Requirement

Demonstrated Performance

SAITO FG-30

Demonstrated Performance

DA- 35

Wingspan

(millimeters)

3075 – 3085 3075 – 3085 3075 – 3085 3075 – 3085

Target Length

(millimeters)

1830 – 1840 1830 – 1840 1830 – 1840 1830 – 1840

Construction Fiberglass airframe/ wood bulkheads

Fiberglass airframe/ wood bulkheads

Fiberglass airframe/ wood bulkheads

Fiberglass airframe/ wood bulkheads

Engine SAITO FG-30 DA-35 SAITO FG-30 DA-35

Engine Location Puller Prop located in front of the target

Puller Prop located in front of the target

Puller Prop located in front of the target

Puller Prop located in front of the target

Internal Design Metalized Wood and Composites Wing

Metalized Wood and Composites Wing

Metalized Wood and Composites Wing

Metalized Wood and Composites Wing

Launch Method Catapult Catapult Catapult Catapult

Recovery Method

Belly land Parachute Belly land Belly land

Table 2: MQM-186 A/B Performance Requirements and Demonstrated Performance

Description Threshold Requirement

Objective Requirement Duration

Demonstrated Performance

SAITO FG-30

Demonstrated Performance

DA- 35

Ground Control System

CloudCap Piccolo or approved equivalent

CloudCap Piccolo or approved equivalent

N/A CloudCap Piccolo SL

CloudCap Piccolo SL

Flight Termination

System

Loss of Ground Control and Loss of GPS

Loss of Ground control and

Loss of GPS

Adjustable to support mission requirements

Loss of Ground control and Loss of GPS

Loss of Ground control and Loss of GPS

Dash Speed 33.4 m/s

(65 knots)

37 m/s

(72 knots)

5 minutes 33 m/s

(67 knots)

39 m/s

(76 knots)

Cruise Speed

20 m/s

(39 knots)

30 m/s

(58 knots)

10 minutes 30 m/s

(58 knots)

30 m/s

(58 knots)

Endurance

(without alternator)

3 hours 4 hours Cumulative Flight Time

45 hrs

(battery limit)

5 hrs

(battery limit)

Payload 12 pounds 20 pounds N/A 14 lbs 18 lbs

Maximum Altitude

(MSL)

3,600 m

(11,810 feet)

5,000 m

(16,400 feet)

1 minute 3,600 m

(16,400 feet)

3,600 m

(16,400 feet)

Cruise Altitude

(MSL)

2,000 m

(6,560 feet)

3,000 m

(9,842 feet)

5 minutes 3,000 m

(9,842 feet)

3,000 m

(9,842 feet)

Low Altitude

(AGL)

500 m

(1640 feet)

500 m

(1640 feet)

30 seconds 500 m 500 m

Operational Range #

(Line-of- Sight)

32 km

(19 miles)

40 km

(24 miles)

N/A 40 km

(24 miles)

40 km

(24 miles)

# The “Line of Sight” requirement refers to the direct communication link between the Ground Control Station and the target. The operational range shall not require any additions or modifications to the Ground Control System (GCS) hardware such as a communications repeater or satellite radio to meet the line-of-sight requirement.

MQM-186 A/B Group 2, Aerial Target Performance Requirements
# The “Line of Sight” requirement refers to the direct communication link between the Ground Control Station and the target. The operational range shall not require any additions or modifications to the Ground Control System (GCS) hardware such as a ...

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