This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Family: Titan. Country: USA. Status: Study.
Proposed Titan upgrade with cryogenic core as replacement for NLS.
SpecificationsLiftoff Thrust: 1,685,960 kgf. Total Mass: 1,138,660 kg. Core Diameter: 6.0 m. Total Length: 72.0 m. Flyaway Unit Cost $: 48.72 million. in 1985 unit dollars.
- Stage Number: 0. 2 x Titan UA1207 Gross Mass: 319,330 kg. Empty Mass: 51,230 kg. Thrust (vac): 725,732 kgf. Isp: 272 sec. Burn time: 120 sec. Isp(sl): 245 sec. Diameter: 3.1 m. Span: 3.1 m. Length: 34.1 m. Propellants: Solid No Engines: 1. UA1207
- Stage Number: 1. 1 x Titan 5 Gross Mass: 500,000 kg. Empty Mass: 45,000 kg. Thrust (vac): 454,500 kgf. Isp: 425 sec. Burn time: 420 sec. Isp(sl): 354 sec. Diameter: 6.0 m. Span: 6.0 m. Length: 60.0 m. Propellants: Lox/LH2 No Engines: 1. PW 1000000 lb LH2
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Last update 12 March 2001.
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© Mark Wade, 2001 .