Russian lunar lander concept, LVPK (original) (raw)

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LVPK

Overview of the LVPK project

(INSIDER CONTENT)


lvpk

LVPK in 2018

(INSIDER CONTENT)


lunar base

Lunar base in 2019

(INSIDER CONTENT)


Russia mulls new-generation lunar lander

Around half a century after a first fruitless attempt to put a cosmonaut on the Moon, a new generation of Russian space engineers embarked on the development of a piloted lunar lander, in accordance with the nation's 10-year space plan starting in 2016. However, unlike the one-seat module of the first Moon Race, the future lander had to support long-term exploration of the Moon and deliver crew anywhere on the lunar surface.

Previous chapter: Lunar base


ortho

Russian lunar lander concept circa 2015.

Read our introductory article on the subject at:

PopMech

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In 2015, after several years of preliminary studies, the Russian space agency, Roskosmos, made plans to begin funding the development of a lunar lander and associated systems which would be necessary to deliver crews from lunar orbit to the surface of the Moon.

In the official documentation, the project was officially identified as Lunar Ascent and Descent Complex, LVPK.

According to the Russian lunar exploration plans circa 2015, the lander would be delivered to the lunar orbit by a dedicated rocket without a crew. It would then rendezvous and dock with a piloted transport vehicle in the lunar orbit. The lander would then deliver the crew to the surface and its ascent stage would carry cosmonauts back to the lunar orbit for a rendezvous with a transport vehicle for trip back to Earth.

Several concepts of the lunar lander were formulated in 2016. At the time, the spacecraft had the following specifications:

Specification Initial version Heavy version
Spacecraft mass in lunar orbit 20 tons 27 tons
Crew size 2 people 4 people
Cargo delivered to the lunar surface 100 kilograms up to 625 kilograms
Flight duration in unmanned mode in lunar orbit 190 days 190 days
Duration on the surface of the Moon with crew 3 days 14 days
Number of supported person/EVAs 4 21
Diameter 5.5 meters 5.5 meters
Length 11 meters 11 meters

Comparison of lunar landers systems:

lm surface Altair lvpk Lander
- LM (Saturn-Apollo) LK lander (N1-L3) Altair (Constellation) Roskosmos (2015) (IC) NASA (2019) (IC)
Liftoff mass 14.67 - 16.37 tons 5.56 tons* 45 tons 20 tons 45 tons****
Crew 2 1 4 3 3
Habitable volume 6.65 cubic meters 5 cubic meters 17.5 cubic meters** 16-25 cubic meters ?
Lunar surface access Equatorial regions, Near side Equatorial regions, Near side Global Global, including polar regions Global, including polar regions
Surface duration with crew 3 days 1 day 4-7 days up to 3 ?
Maximum surface duration without crew Up to 1 A few hours Up to 210 days Up to 14 days*** ?
Payload to the lunar surface Up to 300 kilograms Less than 50 kilograms No less than 500 kilograms No less than 125 kilograms ?
Lunar samples delivered to lunar orbit Approximately 120 kilograms Less than 50 kilograms No less than 100 kilograms No less than 25 kilograms ?
Extra habitable volume No No Airlock No ?

*Not including Block D braking stage; **including airlock; ***Can be extended within lunar base operation; ****includes transfer stage, but does not include refueling tanker.

Lunar lander studies for the Gateway station (2016-2018) (INSIDER CONTENT)

lvpkk

Between 2016 and 2018, Russian industry conducted a new phase of the lunar lander design asociated with the planning for the International Cis-Lunar Platform, a.k.a. the Lunar Gateway. Not coincidently, Korolev-based RKK Energia did its research into the LVPK lander system in parallel with the work of NASA's Lander Study Group then recently formed for looking into lunar expeditions to be staged from the Gateway. (INSIDER CONTENT)

Next chapter: The LVPK program in mid-2010s (INSIDER CONTENT)

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Page author: Anatoly Zak; Last update:May 29, 2025

Page editor: Alain Chabot; Last edit: Sept. 25, 2017

All rights reserved

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LVPK

A notional concept of a lunar lander circa 2010.

Lunar Lander

This artist rendering depicts a concept of a lander used in the early planning of Russian lunar expeditions. The spacecraft is shown in the lunar orbit, preparing for descent on the surface. Click to enlarge. Copyright © 2008 Anatoly Zak


Svobodny region

This artist rendering depicts a concept of a lander on the surface of the Moon. Click to enlarge. Copyright © 2007 Anatoly Zak


LLO


lander

conceptualized during 2015 to be compatible with


LVPK