Notional solid rocket engine. Study 1963. Operational date would have been April 1973 Used on Nova MM 14A launch vehicle. Solid propellant rocket stage. Operational date would have been April 1973. Nova MM 14A first stage.
AKA: Nova MM 14A-1. Status: Study 1963. Thrust: 63,595.00 kN (14,296,724 lbf). Specific impulse: 263 s. Specific impulse sea level: 234 s. Burn time: 106 s. Height: 58.10 m (190.60 ft). Diameter: 7.60 m (24.90 ft).