Detailed Requirements. The Performer shall design, develop, fabricate, test, and deliver eight (8) inert SOPGM Cruise Missiles prototypes and two (2) Captive Air Training Missile (CATM) SOPGM prototypes that meet the following performance requirements: Threshold range of 200 Nm and objective range greater than 400Nm Compatible with the SOPGM Common Launch Tube (CLT) and Battle Management System (BMS) Type-1 data link connection to Situational Awareness Data Link (SADL) (threshold) and SADL/Link-16 (objective). Threshold M-Code Global Positioning System (GPS)/Inertial Navigation System (INS), with an objective to incorporate resilient navigation capabilities for operation in a denied or degraded GPS environment. This system will include at a minimum (threshold) an Electro-Optical/Infra-Red (EO/IR) seeker and as an objective, incorporate a multi-mode seeker package able to acquire and/or reacquire targets in flight. Removable payload section that can accept a minimum (threshold) of 13lbs of warhead or other desired payload with an objective of 37 lbs. Meets a Technology Readiness Level 7 defined as: system prototyping demonstration in an operational environment. Prototype near or at planned operational system. Represents a major step up from TRL 6 by requiring demonstration of an actual system prototype in an operational environment (e.g., in an aircraft, in a vehicle, or in space). The two (2) Captive Air Training Missiles (CATM) shall also fully represent an inert munition (electrical, power draw, weight and center of gravity) to enable simulated launches through the full launch sequence without releasing the weapon. The two CATMs are required for System Integration Lab (SIL) testing and ground and captive carry testing.
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Sources: Prototype Agreement, Prototype Agreement