Photo Gallery - Lunar L3

Media Gallery for Lunar L3
          Short Description
Apollo vs N1-L3 Apollo CSM / LM vs L3 Lunar Complex apolvsl3.gif
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Credit:
© Mark Wade
  Apollo vs N1-L3
LK landing leg View of the landing leg to the cosmonaut's front left. Note the solid rocket motors mounted above each leg that fired DOWN to settle the LK securely on the surface once the lander was near the surface. Yangel OKB tests proved such rockets greatly improved the chances of the rocket not toppling if landing on a 30 degree slope or with one leg on a moon rock. The descent ladder is seen to the right of the picture. lkfrontl.jpg
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Credit:
© Mark Wade
  LK landing leg
LK Overhead Overhead view of the LK lander, showing Kontakt docking system hexagonal grid docking structure. Exit hatch and ladder are to the right; scallop for main view port at front. Two high gain antennae at either side provided transmission of television from the lunar surface to earth. lkoverhd.jpg
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  LK Overhead
N1 Cutaway Dimensioned Russian cutaway drawing of N1 launch vehicle. n1cut4.gif
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  N1 Cutaway
L3 Cutaway Dimensioned Russian cutaway drawing of L3 manned lunar landing complex. l3cut1.gif
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  L3 Cutaway
LOK Orbital Module LOK Orbital Module, view down from top of spacecraft toward Soyuz descent module. lokoml.jpg
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Credit:
© Mark Wade
  LOK Orbital Module
LOK Orbital Module LOK Orbital Module, docking control station. The manoeuvring panel and controls were located where the grey dummy panel is. It is flanked by hand controllers. The cosmonaut would look through the cupola to accomplish manual docking with the LK after its return from the lunar surface. lokome1.jpg
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Credit:
© Mark Wade
  LOK Orbital Module
LK Test Article Subscale dynamic test article of a late configuration of the LK, as preserved in the TsniiMash museum. This shows well the complex shape of the Lunar Cabin and the final LPU configuration. lktstes1.jpg
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Credit:
© Mark Wade
  LK Test Article
S5.51 LOK engine Side view of the twin-chamber Isayev S5.51 engine used in the Soyuz 7K-LOK lunar orbiter. The two smaller chambers of the S5.52 supplemental engine protude beyond the main engine bells to either side. s551b.jpg
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Credit:
© Mark Wade
  S5.51 LOK engine
LOK Block I side View of the LOK Block I. Noticeable are the fragile radiator panels, and the large manoeuvring thrusters at the forward end. The large cylindrical devices are sensors of the attitude control system. loksmsi2.jpg
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Credit:
© Mark Wade
  LOK Block I side
LOK Block I forward View of the dome covering the pressurized instrument compartment of the LOK. loksmfwd.jpg
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Credit:
© Mark Wade
  LOK Block I forward
LOK Descent Module LOK Descent Module and Orbital Module. Note the cupola at the left top of the Orbital Module. On the opposite wall are the lunar mapping camera apertures and control station. lokdmoma.jpg
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Credit:
© Mark Wade
  LOK Descent Module
LOK reaction control The upper half of this item is the ODOP (Orientation and docking engine section) of the LOK, mounted at the top of the orbital module. The cone at top was had grapples for snagging the hexagonal grid of the large disk on top of the LK. Propellants for the orientation and manoeuvring engines were in the tanks in this section. The bottom half of this item is similar to a test installation used on the Soyuz 7K-L1S destroyed in the several N1 launches. lokrcsdm.jpg
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Credit:
© Mark Wade
  LOK reaction control
LOK Orbital Module LOK Orbital Module interior lokomint.jpg
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Credit:
© Mark Wade
  LOK Orbital Module
S5.51 LOK engine The complex plumbing fed numerous smaller attitude control thrusters at the base of the LOK. s551.jpg
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Credit:
© Mark Wade
  S5.51 LOK engine
LOK Orbital Module LOK Orbital Module. Note the far greater amount of external cabling and connecting plates than in the standard Soyuz. lokom.jpg
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Credit:
© Mark Wade
  LOK Orbital Module
LOK Block I side View of the LOK Block I instrument/rocket module. The fragile radiators, arrayed around the main fuel tank, extended away from the body of the spacecraft in flight. The silvery instrument section has numerous patch panels for connecting external wiring. The tapered interstage with stringers connected to the Soyuz descent module. Large 'mooring' thrusters arrayed around this section provided high-authority manoeuvring capability for the LOK in its rendezvous and docking with the LK. loksmsid.jpg
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Credit:
© Mark Wade
  LOK Block I side
LK ladder base Detail of the base of the ladder, showing the battery racks below the ladder. Note the shape of the foot pad. lkdet13.jpg
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Credit:
© Mark Wade
  LK ladder base
Soyuz LOK Soyuz LOK lunar orbiter. soybiglo.gif
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Credit:
© Mark Wade
  Soyuz LOK
LK panels The cosmonauts' view of the LK viewports and control panels. On the left, environmental control and cabin depressurisation controls (light blue panel); radio controls (dark green panel); large porthole looking down at lunar surface during landing. The small porthole looked upward for docking. The optical devices that were associated with these portholes are not present in this mock-up. To the right, sequencer panel for calling up sequences for manoeuvres, landing, rendezvous, and docking. Guarded switches initiated major events. One of two hand controllers is visible below the green radio panel. lkpanels.jpg
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Credit:
© Mark Wade
  LK panels
LK Two View Two view layout drawing of LK lunar lander. lknewbig.gif
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Credit:
© Mark Wade
  LK Two View
Early LK Test Model Dynamic Test Model of Early LK Concept. lkmodel.jpg
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Credit:
© Mark Wade
  Early LK Test Model
LK drawing at Kaluga Cutaway drawing of LK lunar lander, showing position of cosmonaut in cabin. lkkaluga.jpg
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Credit:
e
  LK drawing at Kaluga
LK Detail forward view drawing of the LK lunar lander. lkgood.gif
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Credit:
© Mark Wade
  LK
LK Main Engine The LK engine cluster at the base of the lander. The single chamber RD-858 of the 2,050 kgf main engine is at the centre. It is flanked by the two nozzles of the RD-859 2,045 kgf backup engine. The smaller nozzles are exhaust nozzles for the turbines of the pump-fed engines. At landing or takeoff, both the primary and backup engines would ignite. Only if both engines were operating, would one shut down. The thick clamshell doors closed over the engines after landing to insulate them and prevent ingestion of lunar soil. lkengine.jpg
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Credit:
© Mark Wade
  LK Main Engine
LOK Descent Module LOK Descent Module detail. The ablative material is far thicker than on the standard Soyuz descent module for the re-entry from lunar distances at twice the energy as that from earth orbit. lokdmdet.jpg
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Credit:
© Mark Wade
  LOK Descent Module
LK Overall view of the LK preserved at the Orevo Museum of the Bauman Moscow State Technical University. biglk.jpg
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Credit:
© Mark Wade
  LK
LOK Lunar Orbiter The Soyuz 7K-LOK lunar orbiter spacecraft to be used in the L3 lunar landing project complex. lokkalug.jpg
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Credit:
© Mark Wade
  LOK Lunar Orbiter
Chelomei LK-700 Chelomei LK-700 manned direct lunar landing spacecraft - cruise and landed configurations lk700.jpg
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Credit:
© Mark Wade
  Chelomei LK-700
Soyuz 7K-LOK Soyuz 7K-LOK manned lunar orbit spacecraft. lokdwg.jpg
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Credit:
© Mark Wade
  Soyuz 7K-LOK
Krechet Spacesuit Krechet lunar space suit as displayed at NPO Zvezda. As in the Orlan suit still used on Mir, the cosmonaut entered the suit by swinging open a hatch at the rear. The backpack containing the life support system was housed in the backpack which made up the hatch door. As in Apollo, the gold-coated outer visor of the helmet reflected ultra-violet radiation. The integrated Kretchet design meant that no external hoses were required as in the American Apollo suit. krechet1.jpg
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Credit:
Andy Salmon
  Krechet Spacesuit
Krechet Spacesuit Front view of the Krechet lunar space suit krechet2.jpg
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Credit:
Andy Salmon
  Krechet Spacesuit
 
 
 
 
 
 
 
 
 

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© Mark Wade, 1997 - 2007 except where otherwise noted.

 
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