Hohmann Transfer DeltaV Calculator v.1.0 coming soon!

@YaMomzBox420 cool

@Vedhaspace ∆v1 is the "transfer orbit injection burn" that puts the craft into the transfer orbit. ∆v2 is the "orbital insertion burn" that places the craft into the target orbit. The 3rd one is the total of the first two.

@YaMomzBox420 yeah

@Vedhaspace yeah, I've noticed it varies from 3500 to 4500 depending on the design of the craft(from Droo), so I'm assuming the program is accurate if Droo had no atmosphere

But we need the most accurate burns to actually go there

@YaMomzBox420 yeah

So why are there 3∆v?

@Vedhaspace If you're already in orbit or launching from a planet/moon with no atmosphere then it should be accurate though

@YaMomzBox420 we need nearly 3700 m/sec ∆v for orbit sometimes 3500m/sec ∆v is enough they depends on the drag

@Vedhaspace Not yet, but I'm already looking into implementing that. If you notice in the screenshot it says ~3500 m/s ∆v to reach 100km orbit from the ground, but when I launch the rocket it only drops to ~1200 before it runs out of fuel in a suborbital trajectory. I can account for drag by adding some calculations to the code, but it's complex and relies on information about the crafts shape and size that isn't easy to find using vizzy

Cool!
Does it calculate drag ∆v loses?

@YaMomzBox420 lol weird

@Staticalliam7 When I go to edit the post it shows ∆v in the text box, but when I submit and look here it shows ?v 🤦🤦🤦🤦🤦

∆

@Staticalliam7 lol idk why it keeps doing that to me...🤦 I actually used that symbol and it still fucked it all up

btw here's the delta symbol: Δ