Oct 2, 2001 #1 enkodham Aerospace Joined Jun 2, 1999 Messages 5 Location US I am interested in obtaining information concerning atmospheric drag for a spacecraft in a relatively low orbit. How much more accuracy can I get from using rarified models than by using a traditional acceleration-due-to-drag equation?
I am interested in obtaining information concerning atmospheric drag for a spacecraft in a relatively low orbit. How much more accuracy can I get from using rarified models than by using a traditional acceleration-due-to-drag equation?