Gross Mass: 1,633,000 kg.
Empty Mass: 163,000 kg. Thrust (vac): 2,494,000 kgf. Isp: 263 sec. Burn time: 150 sec. Propellants: SolidIsp(sl): 238 sec. Diameter: 6.1 m. Span: 6.1 m. Length: 34.1 m. Country: USA. No Engines: 1. 240 inch solidStatus: Study NASA, 1960. Comments: Notional solid motor considered in cluster of 4 as alternative to Nova 8 F-1 stage. Led to 260 inch motor tested in late 1960's. .