RFI-Drone CLT

The United States Special Operations Command (USSOCOM) is conducting market research to better understand industry capability and expertise in performing spiral development, engineering services, and production of a SOF-peculiar munition. The project involves designing and manufacturing an air-launch vehicle that can be released from SOF fixed-wing air platforms utilizing the Common Launch Tube (CLT). The vehicle should have a maximum weight of 55 lbs, a diameter of 5.9 inches, and a maximum length of 42 inches. It should also have a passive seeker assembly with integrated Automatic Target Recognition (ATR) and a warhead or payload. The system should be able to operate in a contested environment and have a minimum range of 75NM, a loitering time of 40 minutes, and a cruise speed of 50-100 kts. The project requires a Rough Order of Magnitude (ROM) estimate for initial planning purposes, and white papers should not exceed 10 pages. • The project involves designing and manufacturing an air-launch vehicle for SOF fixed-wing air platforms. • The vehicle should have a maximum weight of 55 lbs and a diameter of 5.9 inches. • The system should have a passive seeker assembly with integrated ATR and a warhead or payload. • The project requires a ROM estimate for initial planning purposes. • White papers should not exceed 10 pages and should be submitted via email to the primary point of contact.