KSR-2 is a planned liquid bi-propellant suborbital launch vehicle. It is the second installment of the KSR Rocket Family, composed of a single stage, fueled by nitrous oxide and methanol. KSR-2 will have a total length of 4 m, a diameter of 0.4 m and a total mass of 591 kg, its apogee will be around 100 km.