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How would I estimate the transfer time between Mars and Saturn if I have more Delta-V than necessary for a Hohmann transfer?

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I whomped up a spreadsheet where you can set perihelion and aphelion of transfer orbit.

Here's a screen capture from the spreadsheet where I set perihelion of transfer orbit at 1 A.U. and aphelion at 12 A.U.

enter image description here

Of course SMA is (perihelion+aphelion)/2. Where the transfer orbit crosses Mars orbit, r is 1.524 A.U.. At Saturn, r is 9.537 A.U.. Knowing a, mu and r you can figure speed using the vis viva equation.

Besides speeds you must also take angle between velocity vectors into account. Incorrectly assuming Mars and Saturn are in circular orbits, that angle would be transfer orbit's flight path angle. Then you can use the law of cosines to get the delta V between vectors.

I am hoping you will examine the cells in this spreadsheet and try to reverse engineer what I did.

Here's a screen capture with some of the relevant numbers emphasized:

enter image description here

You would do well to proofread this spreadsheet. I hastily adapted it from a NonHohmann Earth To Mars spreadsheet. I tried to relabel and replace different quantities like planet radius, gravitational parameter, and so on. But I do make mistakes. I would be grateful if anyone reviewed my efforts.

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