Skyrora Skylark L suborbital research rocket

Skylark L is Skyrora's guided, single-stage suborbital rocket using high-test hydrogen peroxide and kerosene. Its pressure-fed liquid engine has regenerative cooling, while thrust-vector and roll control guide the ascent and coast. Published design specifications give a 50 kg payload and 102 km target apogee; these are design capabilities rather than the result of every flight. The vehicle supports development of Skyrora's larger launch systems.