A threat simulation system for evaluating aircrafe/watercrafd/battle-vehicle survivability equipment, the system comprising the following: a Static Pyrotechnic Unit, SPTU, and a support stand on which said SPTU is positioned, said support stand comprising a base and insulating board connected by a telescopic pole, said insulating board having wires for igniting the SPTU, and said SPTU being coated with a flammable material/compound for electrical ignition; a rocket simulation and launch system comprising a Short Range Simulating Rocket, SRSR, and a rocket launching apparatus, said SRSR comprising a front section, which comprises a pyrotechnic flare material, a back section which comprises a propellant, a rocket engine, and stabilizing fins, and in between the front section and the back section, there is a safety mechanism that enables/disables the activation of the SRSR, said rocket simulation and launch system comprising a tripod that can change azimuth and elevation and a pedestal on top of which a launch tube is mounted; and a control system configured to set the timing of and activates said SPTU and said rocket simulation and launch system, wherein the SPTU is configured so that when the SPTU is ignited, the resulting flash is characterized by having an IR wavelength and multi spectral emission, intensity and time duration that simulates the initial flash created by a fired shoulder missile; and wherein the SRSR is configured so that when the SRSR is fired, the resulting radiation is characterized by having an IR wavelength and multi spectral emission, intensity and time duration that simulates the radiation trail emitted from a fired shoulder missile; wherein, the flash created by the SPTU, and the trail emission of the SRSR are detectable by the aircraft/watercraft/battle-vehicle survivability equipment and the trajectory and trail emission characteristics and trajectory of said trail emission of said SPTU and said SRSR can be determined. a Static Pyrotechnic Unit, SPTU, and a support stand on which said SPTU is positioned, said support stand comprising a base and insulating board connected by a telescopic pole, said insulating board having wires for igniting the SPTU, and said SPTU being coated with a flammable material/compound for electrical ignition; a rocket simulation and launch system comprising a Short Range Simulating Rocket, SRSR, and a rocket launching apparatus, said SRSR comprising a front section, which comprises a pyrotechnic flare material, a back section which comprises a propellant, a rocket engine, and stabilizing fins, and in between the front section and the back section, there is a safety mechanism that enables/disables the activation of the SRSR, said rocket simulation and launch system comprising a tripod that can change azimuth and elevation and a pedestal on top of which a launch tube is mounted; and a control system configured to set the timing of and activates said SPTU and said rocket simulation and launch system, wherein the SPTU is configured so that when the SPTU is ignited, the resulting flash is characterized by having an IR wavelength and multi spectral emission, intensity and time duration that simulates the initial flash created by a fired shoulder missile; and wherein the SRSR is configured so that when the SRSR is fired, the resulting radiation is characterized by having an IR wavelength and multi spectral emission, intensity and time duration that simulates the radiation trail emitted from a fired shoulder missile; wherein, the flash created by the SPTU, and the trail emission of the SRSR are detectable by the aircraft/watercraft/battle-vehicle survivability equipment and the trajectory and trail emission characteristics and trajectory of said trail emission of said SPTU and said SRSR can be determined.