The invention relates to the technical field of heat pump equipment, in particular to a superconducting missile type air energy source heat pump unit system. The superconducting missile type air energy source heat pump unit system comprises a heat pump type compressor, a four-way valve, a special efficient heat exchanger, filters, an electronic expansion valve, a diversion head, an evaporator, a plate type heat exchanger, a missile-shaped subsonic-speed heating part, superconducting liquid, a gas-liquid separator, a fan, an airtight pipeline, a water inlet, a water outlet and an insulating water tank. The application range of the superconducting missile type air energy source heat pump unit system is widened to the areas in the south and the north, heat, cool air and hot water can be supplied, the product performance is safe and reliable, and use is convenient. In addition, experiments prove that the heat efficiency is far higher than that of an existing air energy source heat pump water heating unit under the ultralow-temperature working condition, and under the ultralow-temperature condition, the heat efficiency is not attenuated or slightly reduced, and the energy saving effectis very obvious.