S102
S‑102 is a two‑stage sounding rocket developed by the United States National Aeronautics and Space Administration (NASA) for atmospheric and space science research. The vehicle was designed to carry small scientific payloads to sub‑orbital altitudes of approximately 250 kilometres, enabling experiments that require brief periods of microgravity and studies of the upper atmosphere and near‑space environment. Construction of the S‑102 began in the early 2010s as part of NASA’s efforts to provide cost‑effective, high‑frequency launch opportunities for university and industry research teams. The rocket is built around a first stage using a solid‑fuel motor and a second stage that provides the final boost to target altitude. Its overall length is about 12 metres (39 feet) and it can lift payloads of around 200 kilograms (440 pounds) in a single flight.
The S‑102 has been launched from several U.S. launch sites, including White Sands Missile Range in New