Your spacecraft is in an. initial 200 km altitude circularearth orbit. Performing a Hohmann transfer compute:
a) the TOTAL delta-v required for a Hohmann transfer to a 1000 kmaltitude coplanarcircular earth orbit.
b) What is the transfer time in minutes?
Your spacecraft is in an. initial 200 km altitude circular earth orbit. Performing a Hohmann transfer compute: a) the TO
-
- Site Admin
- Posts: 899603
- Joined: Mon Aug 02, 2021 8:13 am