The Tan-SAM 1 missile is cruciform in cross section with four clipped delta wings attached to the mid body, and four small steerable clipped delta fins at the rear of the missile. The missile is propelled by a
solid rocket motor, with giving it a burn-out velocity of about
Mach 2.4. It is initially
inertially guided to a likely intercept point, with an
all-aspect infra-red seeker taking over to handle terminal guidance. The missile has a 9.2-kilogram fragmentation warhead triggered either by contact or a radar proximity fuze with a lethal radius of between 5 and 15 meters depending on the target type. A fire unit consists of one Fire Control System vehicle and two launcher vehicles as well as a number of support vehicles with a total crew of fifteen men. The Fire Control Systems vehicle consists of an
Isuzu 6×6 truck with a 30 kW
generator unit mounted behind the driver's cabin, and a rectangular three-dimensional
pulse-doppler phased array radar. The radar can operate in three modes: omni-directional search, sector search/course tracking mode, and fine tracking mode. The radar is scanned both mechanically and electronically and can track up to six targets within the same 110-degree arc in course tracking mode. Two targets can be tracked in fine tracking mode at greater accuracy, with the single-shot kill probability for each target relayed to the operator via a
CRT display. The radar has a range of about 30 kilometers, and has built in IFF capabilities. Information on the two selected targets is then passed to the two attached launcher units, which are also mounted on Isuzu Motors 6×6 trucks, which slew and elevate their launchers toward the target. The launchers can be deployed up to 300 meters away from the Fire Control System vehicle. An intercept course is computed for the missile, and the
missile is launched. The missile follows the initial inertial course until it reaches a pre-programmed point where it activates its infrared seeker. The infrared seeker only scans a programmed area of the sky to prevent it from locking onto the sun. From that point it switches to passive infrared homing for the terminal phase of the flight. The infrared seeker does not use IR filters to reject decoys, although there is a degree of protection provided by the use of intermediate frequency seeker scanning pattern. Each launcher is equipped with an optical director that can be used instead of the radar in a high ECM environment or if the radar is not operational; additionally the vehicle can be mounted with one or two 12.7 mm calibre
heavy machine guns, for self-defense in frontal forward areas against ground threats and close-in(<500 m) incoming air threats. The system can be set up in approximately 30 minutes, and the launcher reload time for all four missiles is around three minutes. SAM-1C upgraded missile use a phased array active radar seeker, with the capability of receiving mid-course guidance updates from the Fire Control Systems vehicle. The upgrade also increases the missile's maximum range to 14 kilometers while increasing the missile weight to 105 kilograms. A new smokeless motor with improved thrust is also fitted, replacing the existing motor. Also the Fire Control Systems vehicle is fitted with a
thermal imager to improve operation in an
ECM heavy environment. ==Deployment==