Powered Flight from Earth to Mars - Find Help Here

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The discussion centers on the complexities of powered flight from Earth to Mars, particularly how orbits differ from unpowered flight. Users emphasize that powered trajectories require numerical methods for calculation, as traditional conic sections do not apply. The conversation highlights various propulsion methods, including ion drives and chemical rockets, and the implications of continuous thrust on flight dynamics. Participants express interest in both constant acceleration scenarios and multistage powered flight options. The need for specific trajectory calculations in powered interplanetary travel is a key focus.
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lemme start of by saying hi...

i came across this forum on a search in google and found it nice...

i got a nice problem that i cud use help on

we all know the ususal orbital mechanics of the conic sections. this type of orbit occurs only in unpowered flight (where u don't use any engines, just use the gravity field of planets)

what wud the orbits be like if the flight was powered.

im looking at interplanetary powered flight say from Earth to mars.

anyone has already done this or know how todo this... help!

thx
 
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Hi revenant, welcome to PF!

AFAIK it needs to be done numerically.

There is probably something out there somewhere. Look up trajectories relating to 'ion drives' which are continuously powered spacecraft .
 
Are you interested in a trickle accelleration, like from an ion engine, or a quick flight where you're accelerating at 1g for half your flight, and decelerating at 1g for the second half?
 
well... the type of engine is chemical rocket/electrical/ion... that is i can use them all or just one of them or any two of them... its basically multistage and its powered flight. so u have thrust coming in the force equation and its no longer conic, angular momentum is also not conserved!
 
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