I normally rely on BurnTime MFD to tell me how much Dv a spacecraft can deliver, but I am currently stacking up some Velcro stages and BT MFD shows Dv for each individual vessel, without adding the mass of the stages attached above. (Clever Velcro does include the mass of attached vessels, so the attachments do effect performance.)
I suppose I could briefly reconfigure each stage, adding the mass of upper stages and payloads, and then use BT MFD to get a true reading of Dv. Then again, it might be time to learn something new.
I found the Tsiolkovsky rocket equation at http://en.wikipedia.org/wiki/Rocket_equation which seems simple enough:
Dv = Ve In m0/m1
Ve is the exhaust velocity Isp * g (which is simply the Isp figure used in Orbiter)
m0 is the mass of the vehicle including fuel
m1 is the empty mass of the vehicle
But the wiki article does not define In. Perhaps it is some common function known to all math wizards and needing no further explanation --like the "equal" sign and "division" slash -- except for dolts like me.
Anyone willing to tutor a math moron?
I suppose I could briefly reconfigure each stage, adding the mass of upper stages and payloads, and then use BT MFD to get a true reading of Dv. Then again, it might be time to learn something new.
I found the Tsiolkovsky rocket equation at http://en.wikipedia.org/wiki/Rocket_equation which seems simple enough:
Dv = Ve In m0/m1
Ve is the exhaust velocity Isp * g (which is simply the Isp figure used in Orbiter)
m0 is the mass of the vehicle including fuel
m1 is the empty mass of the vehicle
But the wiki article does not define In. Perhaps it is some common function known to all math wizards and needing no further explanation --like the "equal" sign and "division" slash -- except for dolts like me.
Anyone willing to tutor a math moron?