Unless Bosanac has a last minute change, the paper is done!
This commit is contained in:
@@ -121,7 +121,7 @@
|
||||
|
||||
The mission begins in late June of 2024 and proceeds first to an initial gravity assist with
|
||||
Mars after three and one half years to rendezvous in mid-December 2027. Unfortunately, the
|
||||
launch energy required to effectively used the gravity assist with Mars at this time is
|
||||
launch energy required to effectively use the gravity assist with Mars at this time is
|
||||
quite high. The $C_3$ value was found to be $60.4102 \frac{\text{km}^2}{\text{s}^2}$. However,
|
||||
for this phase, the thrust magnitudes are quite low, raising slowly only as the spacecraft
|
||||
approaches Mars, allowing for a nearly-natural trajectory to Mars rendezvous. Note also that
|
||||
|
||||
Reference in New Issue
Block a user