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The 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)[reply]
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)[reply]
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