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Russia's future spacecraft and many little-known historic projects are described in unprecedented detail in a richly illustrated book to be published in 2013. Contact the author for details.

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Above: A two-part Mars sample return spacecraft proposed around 2008 consisted of a Mars orbiter and a Mars lander. In turn, the lander contained a descent and ascent vehicles, while the orbiter carried an Earth-return vehicle. Credit: IKI

Previous chapter: Luna-24 sample return mission


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Project 5NM

The earliest Soviet plans for delivering Martian soil naturally grew out of similar missions to the Moon developed in the second half of the 1960s at the NPO Lavochkin design bureau led by Georgi Babakin. At the beginning of 1970, Babakin directed his engineers to prepare a technical proposal for a Martian sample return mission. By the summer, the team had already formulated a concept of the spacecraft designated 5NM. According to the plan, the yet-to-be-operational N1 heavy-lifting rocket would launch a 98-ton behemoth into the low-Earth orbit in September 1975. From there, the fourth stage would accelerate a 20-ton spacecraft on its way to Mars.

Similarly to the Soviet lunar exploration program, the Martian sample return mission would be preceded to the Red Planet by the 4NM rover in 1973. However both missions had to be ultimately postponed and scaled down, because the N1 rocket never "learned to fly." To fit the mission, renamed 5M, into the smaller Proton rocket, the soil-sampling spacecraft was split into three vehicles which would rendezvous in the Earth orbit and in the Martian orbit. Again, the complex 5M soil-return mission would be preceded by a one-way trip to Mars of the 4M rover.

After several changes, the preliminary design of the 8,700-kilogram 5M vehicle was completed in January 1976. The spacecraft was to use an umbrella-like braking device expanding to a diameter of almost 12 meters to break itself in the Martian atmosphere. By 1978, the first prototype of the spacecraft and its components were built, however the project was deemed too expensive and complex for full-scale development at the time. (633) The troubled program reportedly caused a significant delay in the last Soviet mission to bring soil samples from the Moon, as well as contributed to a decision to cancel the launch of the Lunokhod-3 lunar rover and disrupted pre-flight tests of Venera-11 and Venera-12 landers.

Still, low-level work on the project continued. Since one of the main challenges of the sample return mission was the need to deliver a large return rocket onto the surface of Mars, Soviet engineers mulled various ways of increasing the capabilities of the lander. During the 1980s, NPO Lavochkin in cooperation with the industry's main research institute -- TsNIIMash -- conducted a multi-phase research project code-named Zarya ("dawn"). Its participants looked at the possibility of using the atmospheres of destination planets as a braking medium during interplanetary voyages as an auxiliary to rocket propulsion.

Post-Soviet plans

By 1990, NPO Lavochkin's planners favored a cone-shaped vehicle that would be capable of active aerodynamic maneuvering in the Martian atmosphere in order to dissipate its speed and thus reduce the need for braking propellant. Not exceeding two tons in mass, the lander would sport 12 deployable petals, three of which would be used for aerodynamic steering during the descent through the Martian atmosphere. The remaining petals would open during the cruise flight in space to expose solar panels, attitude-control thrusters and navigation sensors. The lander code-named Berkut could become the basis for other deep-space missions tasked to penetrate the atmospheres of other planets, such as Jupiter or Venus.

To send soil from Mars to Earth, a three-stage return vehicle would be employed. Its third stage carrying a small capsule for delivering samples to Earth, could be flight-tested during a planned mission to Phobos.

Thanks to its maneuvering capabilities and the latest advances in avionics, the entire Mars-bound sampling spacecraft would be light enough to fit into the existing Proton or even Zenit-3SL rocket. (see appendix)

Berkut project

With the economic recovery in Russia in 2000s and the gradual re-birth of the deep-space exploration program in the country, the return of samples from Mars once again appeared on the long-term agenda of Russian planetary scientists. As a milestone toward this goal, an attempt would be made to return samples from the Martian moon Phobos within the Phobos-Grunt mission ("grunt" is the Russian for soil). It would pave the way to a much more ambitious Mars-Grunt project. However, following the spectacular loss of Phobos-Grunt in 2011, the joint Russian-European ExoMars mission took over the role of technological bridge to the Mars sample-return mission. The ExoMars could also form the foundation for an international effort to reach this goal.

Soyuz-launched mission

A new vision of post-Soviet designs of the Martian sample-return spacecraft emerged in 2004 from the Babakin space center, the newly-formed development arm at NPO Lavochkin. The organization devised a two-part mission that could be launched by a pair of Soyuz-2/Fregat rockets as early as 2016. The first vehicle would carry a Mars lander equipped with an ascent stage designed to lift between 100 and 200 grams of samples from the Martian surface to the orbit of the planet. There, it would link up and transfer samples to an orbiter featuring an Earth-return stage. In this incarnation of the project, the lander would use a giant inflatable heat shield to enter the Martian atmosphere. (391)

Proton-launched mission

By the middle of 2000s, it was deemed affordable to launch the Mars sample-return spacecraft on a single Proton rocket or on its future replacement - Angara. A concept proposed in 2008, called for the delivery of a 5,200-kilogram rover with 210 kilograms of payload to the Martian surface in 2016. During its three-year mission, dubbed Expedition-M, the rover would collect and store samples for a pickup by a return vehicle launched in 2018. Both spacecraft would be based on the Flagman spacecraft bus developed for the Phobos-Grunt project. Despite an optimistic launch dates in the proposal, the actual budget request submitted to the government in 2008 did not expect the launch of Expedition-M before 2022. This timeframe coincided with schedules drafted by NASA and European planners for the same type of mission.

A concept presented in 2010 relied on a single Angara-5 rocket launching a six-ton dual spacecraft, featuring a cruise stage propelled by electric engines. It would be powerful enough to carry a two-part vehicle on a single flight. As in the previous concept, the lander would deliver a return rocket to the Martian surface, where it would be loaded with samples and then blast off back to the orbit of Mars. There, it would rendezvous with the orbiting vehicle. After the transfer of samples, the return carrier would head back to Earth. As of 2010, the mission was optimistically targeted for launch in 2018, following Phobos-Grunt in 2011 and Mars-NET in 2016. However during 2012, all plans for such a mission were pushed back toward the mid-2020s, after the completion of the ExoMars 2018 project and a possible repeat of the Phobos-Grunt mission. Moreover, all soil-returning procedures were now planned to be rehearsed during dedicated lunar missions at the end of the 2010s. Under such a scenario, the landing platform developed in Russia for the ExoMars 2018 mission could be modified for delivering a soil-carrying return vehicle. In the meantime, sample-collecting techniques developed for the Luna-Grunt project could be then applied to Mars missions.

As of 2012, the most optimistic scenarios expected an international sample-return mission in 2022-2024. Other estimates predicted the mission in the second half of the 2020s.


Next chapter: Manned expedition to Mars

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Berkut Mars vehicle for sample return (circa 1990s-2000s):

Launch mass
4,750 - 5,200 kilograms
Lander mass on the surface of Mars
1,700 kilograms
Service module dry mass
500 kilograms
Mars ascent rocket mass
600-700 kilograms
Earth return capsule mass
25-40 kilograms
Launch vehicle
Proton, Zenit (or dual Soyuz-2 launch)


Russian Mars soil-sample return mission concept (Mars-Grunt) as of 2010-2011:

Launch vehicle
Angara-5 (with Briz-M upper stage)
Spacecraft mass
6,040.0 kilograms
Orbiter payload mass
50.0 kilograms
Lander payload mass
20.0 kilograms
Mass of returned soil samples
0.2 kilograms



Text by Anatoly Zak; Last update: January 28, 2017

Page editor: Alain Chabot; Last edit: March 14, 2013

All rights reserved


Lunar soil

Sample of lunar soil delivered by Soviet spacecraft. Copyright © 2011 Anatoly Zak


A Mars sample-return vehicle designed to be launched by the N1 rocket. Credit: NPO Lavochkin


The 4NM lander with a rover was to play a critical role in the Mars sample return mission. Credit: NPO Lavochkin


The 5M lander. Credit: NPO Lavochkin



The 4,750-kilogram Mars sample return vehicle, apparently dubbed Berkut, was designed to fit into a single Proton rocket. Credit: NPO Lavochkin

Babakin lander

return craft

Mars sample-return vehicle (top) and the Mars orbiter proposed by Babakin center at the turn of 2000s. Credit: Babakin center


An inflatable heat shield would be used to deliver the soil-sampling vehicle to Mars. Credit: Babakin center


An ascent stage (right) links up with an orbiter in the orbit of Mars to transfer soil samples for their return to Earth as envisioned by Russian engineers around 2004. Credit: NPO Lavochkin


Around 2008, planners once again considered sending a rover ahead of the sample return mission. Credit: NPO Lavochkin



A depiction of a single-spacecraft Mars sample return vehicle circa 2011. Credit: NPO Lavochkin

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