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Units and values for Isp
editThe specific impulses given here are far too low to be correct. In units of newton-seconds of impulse per kilogram of propellants, the vacuum Isp should be roughly 3,000, like other pressure-fed bipropellant rockets designed for vacuum use. Karn (talk) 09:06, 29 March 2012 (UTC)
- Who uses those units ? "seconds" is traditionally lbf-seconds/lb of prop, or just use exhaust speed in m/s (which matches your n.s/kg). - Rod57 (talk) 18:24, 28 April 2021 (UTC)
Table for variants
editCould have table of variants - with columns for Isp, propellant, and vehicles used in. - Rod57 (talk) 18:19, 28 April 2021 (UTC)
What alloys used
edit- What alloys and structure used in the combustion chamber ?
- What alloy for the nozzle bell ? Some articles (and sources) just say "a niobium alloy". - Rod57 (talk) 19:13, 30 November 2023 (UTC)