The Luna-Glob lander

The Luna-Glob spacecraft (a.k.a. Luna-25 or Luna-Glob-1), promised to be the first Russian lunar lander since the Luna-24 mission launched in 1976. It was expected to land near the South Pole of the Moon and search for water, volatile and organic compounds in the lunar soil during at least a year-long mission.

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A scenario of the Luna-Glob lander mission, as it was envisioned by the end of 2011. The cruise to the Moon was expected to take 12 days. Credit: Roskosmos

On Nov. 17, 2011, the Space Council within the Russian Academy of Sciences, RAN, formally confirmed that Luna-Glob and Luna-Resurs missions had to be split into separate landing and orbiting missions. However despite a common sense of launching an orbiter ahead of the lander, Russian planners had to go with the landing mission first. According to industry sources, by 2012, the propulsion system and tank structure for the Luna-Resurs mission already appeared in metal, along with a number of other components of the lander. However in the process of its development, the Luna-Resurs lander gained weight from the originally projected 1,275 to 1,450 kilograms, reportedly taking it beyond the capabilities of the Indian GSLV II rocket that was suppose to launch it along with an Indian-built orbiter. As a result, it was decided to complete the landing vehicle under the name Luna-Glob lander (a.k.a. Luna-Glob-1 or Luna-25) and launch it separately on a Soyuz-2/Fregat rocket in November 2015 or in the summer of 2016. The manufacturing of the rocket for the mission was completed during 2012, according to TsSKB Progress in Samara. Luna-Glob would take off from a brand-new pad in Vostochny in the Russian Far East, the company said.

In the meantime, the Indian-built Chandrayaan-2 orbiter was left to be launched on the Indian GSLV Mk.2 rocket.

By the beginning of 2012, the Luna-Glob project was reverted to the preliminary design phase. As of July 2012, Russian scientists were apparently still evaluating whether to send the lander to the South Pole or to the North Pole of the Moon, however other sources predicted that the vehicle would land near the South Pole. The Luna-Glob lander would carry only minimum scientific payload with its official main goal being the testing of landing techniques. There were reports that in addition to the primary Russian-built landing system, the Luna-Glob lander would also carry a European-built secondary landing control system, which could be tested during the mission. However, at least one Russian source was skeptical about the reality of reaching a workable agreement with Europe within remaining timeframe.

In its initial incarnation, the landing system would enable Luna-Glob to touch down on the Moon with an accuracy of just around 30 kilometers, IKI scientist Igor Mitrofanov told RIA Novosti news agency in October 2013. According to Mitrofanov, the Boguslavsky Crater near the South Pole of the Moon was considered as a model landing site, however Russian scientists were not expected to choose the final landing site for another two years. The Boguslavsky Crater satisfied both engineering limitations of the mission and, simultaneously looked promising scientifically based on data about the concentrations of water.

With a European system, which could be integrated into the follow-on Luna-Resurs mission, the landing accuracy could be improved to just three kilometers, Mitrofanov said.

As a silver lining for numerous delays of the Luna-Glob, it was possible to develop a demonstrator of the European landing system, known as Pilot-D, for installation on the lander.

As of 2011, the 1,450-kilogram Luna-Glob lander was expected to deliver around 30 kilograms of scientific instruments onto the surface of the Moon, however by October 2012, this payload was reduced to 17-19 kilograms, comparing to 34.5 kilograms onboard Luna-Resurs lander. By January 2013, around 15 instruments were expected to survive the cut. In addition to solar panels, the spacecraft was expected to feature a radio-isotope power generator, RITEG, developed at the nuclear research center in Sarov and a small robotic arm carrying scientific instruments. The spacecraft was expected to survive on the surface of the Moon for at least a year.

The Luna-Glob mission would pave the way to a more sophisticated Luna-Resurs lander scheduled for launch in 2017. (598) However by 2014, the Luna-Glob mission slipped to 2019, pushing Luna-Resurs into 2020s. During the same year, Roskosmos drafted a new Federal Space program, which would extend from 2016 to 2025. According to the document, Luna-Glob landing mission would require 2,980 million rubles. At the time, it was expected that the spacecraft would be functioning on the Moon for a year. (713)

Post-Phobos-Grunt revisions in 2012

Following the Phobos-Grunt launch fiasco, all planetary exploration and science projects in Russia faced uncertain future. Luna-Resurs and Luna Glob missions were now not expected before 2016-2017. According to unofficial sources, both projects were reverted back to the experimental phase, making it likely another major redesign of the missions. During 2012, it looked like orbital and landing mission were split into separately launched vehicles and by June of that year, it was decided that the orbital vehicle would fly first as early as 2016, followed by the landing mission around 2017.


Science instruments proposed for lunar landing missions in 2015 and 2017 (598):

No. Instrument
Mass, kg
Location on lander
1 Radio beacon
Provides high stability radio signal
Main instrument deck
2 TV camera (TVRPM)
Imaging navigation of the robotic arm
Robotic arm
Infra-red spectrometry of minerals
Robotic arm
4 Chemical analysis suite
Chromatographic and mass spectroscopy analysis of volatiles content and chemical composition
Main instrument deck
IKI and University of Bern
Laser mass spectrometer
Main instrument deck
IKI and University of Bern
6 TV spectrometer
UV and optical imaging of minerals with UV excitation
Main instrument deck


Active neutron and gamma-ray analysis of regolith composition


Secondary instrument deck




Radio measurements of temperature of subsurface regolith


Secondary instrument deck




Measurements of dust and micrometeorites


Secondary instrument deck




Measurements of seismic activity


Main instrument deck



ARIES (Luna-Resurs only)

Measurements of plasma and neutrals


Main instrument deck



TERMO (Luna-Glob only)

Direct measurements of thermal properties of regolith


Main instrument deck



LINA (Luna-Glob only)

Measurements of plasma and neutrals


Main instrument deck

IKI and ISP (Sw)


Panoramic and stereo TV system

TV imaging of panoramas and area near lander (rover and robotic arm)


Main instrument deck



Retro reflector

Moon libration and ranging experiment


Main instrument deck



Next chapter: Luna-Glob status in 2014 and 2015


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Written and illustrated by Anatoly Zak

Last update: September 7, 2022

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A Luna-Glob lander under a payload fairing of the Soyuz-2/Fregat rocket, as it was envisioned in 2012. Credit: Roskosmos


Key components of the Luna-Glob lander as of 2012. Credit: IKI


A scale model of Luna-Glob lander presented at the Paris Air and Space Show in Le Bourget in June 2013. Copyright © 2013 Claude Mourier


Luna-Glob on the surface of the Moon as envisioned in 2015. Click to enlarge. Credit: NPO Lavochkin


Demo version of the Luna-Glob lander and a Fregat-SB space tug. In reality, Luna-Glob will fly on a basic Fregat stage without an additional propellant tank seen at the bottom of the structure. Click to enlarge. Credit: Roskosmos


A likely prototype of the Luna-Glob lander under assembly at NPO Lavochkin circa 2015.


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