I know that ESA is cooperating with Roscosmos on the ExoMars project. But what were the reasons of selecting a Proton launch vehicle instead of Ariane? Is it because Baikonur is a more favourable launch site (than French Guyana)?

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    $\begingroup$ I suspect it reflects more on the way the cost of the mission is divided between the two parties. I see they're using a Proton instead of a Soyuz: esa.int/Our_Activities/Space_Science/ExoMars/… $\endgroup$ – Hobbes Mar 14 '16 at 11:19
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    $\begingroup$ Baikonur is not better than Guyana, the latter being closer to the equator and launches over the ocean (although weather is better at Baikonur). I think it is because the US left the ExoMars cooperation with ESA some years ago, and the US part was to deliver launch vehicles and a rover. Russia was simply chosen as replacement of the parts which the US was supposed to have done, probably because then ESA wouldn't need to increase its budget for participating in the mission (by much). And because Russia maybe wouldn't accept any smaller part. They do know alot about launchers. $\endgroup$ – LocalFluff Mar 14 '16 at 13:21
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    $\begingroup$ Also, proton is quoted as twice cheaper (and less powerful than Ariane 5). Why fly an expensive rocket when you just need a cheaper one ? It seems unlikely that Baikonur would be a more favorable launch site since Kourou is closer to the equator. $\endgroup$ – Antzi Mar 14 '16 at 13:22
  • $\begingroup$ @LocalFluff: Arianne can deliver a bigger payload to high orbits. They have about the same max payload capacity (structural durability, fairing size, etc), but Arianne has more delta-V - to reach the same distant destinations of Arianne, Proton-M must make sacrifices in payload mass carried. Or, if they both arrive at LEO with about the same (maximum) payload, Arianne will have a plenty of fuel left. Check their payloads to GTO instead of to LEO. $\endgroup$ – SF. Mar 14 '16 at 14:28
  • $\begingroup$ @SF I've seen those numbers but don't understand how they add up. I and others have asked about those tons to LEO/GEO/X numbers before, and the answer seems to be that it depends... Ariane 5's fuel left in LEO is included in mass to LEO, which is often stated as similar or higher for Proton. $\endgroup$ – LocalFluff Mar 14 '16 at 14:42

As @Antzi said in his now-deleted answer, initially ExoMars was to be a collaboration between ESA and NASA, with NASA providing the launches. When NASA left the program, ESA sought a new deal, this time with Roscosmos.




Despite initial misgivings (Russia had phased out Proton for scientific missions), they agreed after all:



Baikonur is definitely less favorable launch site than Guiana, with highly inclined orbits, but that doesn't play such a big role with interplanetary missions as inclination correction on very high orbits is relatively inexpensive.

But first, there are simple, direct budget concerns: ExoMars doesn't require the large payload capacity of Arianne (and it's difficult to share payload space with commercial missions on an interplanetary launch), and then Proton-M cost per kg to orbit is significantly lower - almost half the price of Ariane 5ES.

And then - considering that Roscosmos provides the launchers, the only costs of ESA are development of the actual payloads. Surely Roscosmos wouldn't be willing to fund an Arianne launch instead...


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