Particular impulse subsequently has deep impacts to the achievable delta-v and linked orbits achievable, and (via the rocket equation) mass portion required to realize a presented delta-v. Optimizing the tradeoffs involving mass fraction and unique impulse is one of the elemental engineering problems in rocketry. If you prefer a https://griffinuensu.smblogsites.com/32779686/the-5-second-trick-for-ispace-casino