Lunar_Lander
New member
Thanks for the additional material. The graphs are interesting, because it is a bit difficult to compare them to other rockets, because the data for them usually gives a LEO and a GTO value. Here we have data for several Elliptical and Circular orbits, again split into Equatorial and Polar...
So let's see, I think I will take the Equatorial curve at 200 km to compare to other vehicle's LEO payload. The rockets I pit the Europa II against are those which were in use in 1971, when it flew on F11.
So:
Europa II 1350 kg
Delta N 998 kg
SLV-3C Centaur 4500 kg (into 185 km Orbit)
Titan 3B 3600 kg (into an Orbit inclined to 28.8°)
Proton 3 19.6 tons
I omitted Rockets like the Scout B because they could only carry 300 kg into LEO, and several Russian Rockets, because for instance the Molnya MK II had only data for payload into the Molnya orbit, while the Vostok MK II only had data for a 850 km orbit. So the Europa II was about to be a Delta-Class vehicle.
So let's see, I think I will take the Equatorial curve at 200 km to compare to other vehicle's LEO payload. The rockets I pit the Europa II against are those which were in use in 1971, when it flew on F11.
So:
Europa II 1350 kg
Delta N 998 kg
SLV-3C Centaur 4500 kg (into 185 km Orbit)
Titan 3B 3600 kg (into an Orbit inclined to 28.8°)
Proton 3 19.6 tons
I omitted Rockets like the Scout B because they could only carry 300 kg into LEO, and several Russian Rockets, because for instance the Molnya MK II had only data for payload into the Molnya orbit, while the Vostok MK II only had data for a 850 km orbit. So the Europa II was about to be a Delta-Class vehicle.