Link for quiz 3

AIDC WEEK 1 OL 3

pls copy link and paste in browser

https://forms.gle/nAcmYdp255vh2H2B7

Comments

Post a Comment

Popular posts from this blog

Satellite Orbital Mechanics

Image
Satellite Orbital Mechanics Quiz Q.1)  Orbit has eccentricity of 0.15 and semi major axis of 9000 km. Determine Periodic time and Apogee height. Q.2)  For a satellite perigee & apogee height is 300 km and 42000 km respectively. Find velocities at apogee & perigee by assuming earth radius 6378 km. Q.3)  Sum & difference of apogee and perigee distances are 50000 km & 30000 km for a certain elliptical satellite orbit. Determine eccentricity. Q.4)  If apogee height and perigee height is of 39342 km & 613 km. Determine semi major axis & eccentricity.                                                                                                                 (Src : Satellite Comm. – R P khan) Link To Submit Answers Orbital Mechanics Answer Submission
Read more