SOYUZ-TM 14, also known as Soyuz TM-14, is a crewed spacecraft launched on March 17, 1992, from the Tyuratam (Baikonur) Space Center using a Soyuz-U2 launch vehicle from Launch Pad LC1. The satellite has dimensions of 7.2 meters in length and 2.2 meters in diameter with a span of 10.6 meters. It was manufactured by NPOE, its dry mass is 2850 kg which matches its launch mass, indicating no fuel or other expendables were loaded post-launch for this mission. The spacecraft is equipped with 2 deployable fixed solar arrays and batteries for power supply. Its design includes a sphere, cone, cylinder, and two panels, and it utilizes the KTDU-80 (S5.80) motor. The satellite's mission was to serve as a crewed spacecraft and it was operated by NPOE, with its payload being Soyuz 7K-STM No. 64.