 | Krechet Spacesuit Credit - Andy Salmon
| Class: Manned. Type: Space Suits. Nation: Russia. Manufacturer: Zvezda. The Krechet spacesuit was designed by the Zvezda OKB for use on the lunar surface. It consisted of flexible limbs attached to a one-piece rigid body / helmet unit. The suit was entered through a hatch in the rear of the torso. The exterior of the hatch housed the life support equipment. Maximum operation time was ten hours.
As in the Orlan suit still used on Mir, the cosmonaut entered the suit by swinging open a hatch in the hard abdomen of the suit at the rear. The backpack containing the life support system was integrated with the hatch. 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.
Krechet Chronology - 1968 March 20 - Lunar spacesuit review. - Program: Lunar L3.
Meeting with Gay Ilyich Severin. Two spacesuits are being developed for the L3 program: the Krechet-94 and Orlan. Both have been in development for two years. The Krechet-94 will allow six hours of lunar surface activity, the Orlan, 2.5 hours. Both weigh about 90 kg. There are consumables for a total of 52 hours of life support in the LK and the LT Lunar Cart. Kamanin feels the suits are too heavy, due to Mishin's demand for a 5 km range from the LK over a three day traverse with the LT. Severin could have instead developed the spacesuit used by Leonov to have a four hour autonomous operation, but Mishin insisted on doubling of the capacity.
- 1968 December 16 - Lunar Soviet. - Program: Lunar L1, Lunar L3.
 | Krechet Spacesuit Front view of the Krechet lunar space suit... Credit- Andy Salmon |
In a four-hour meeting, a number of issues are dealt with. First point was military control of the KIK control centre for lunar missions. A civilian mission control centre is requested. Next, the issue of recovery of L1 and L3 capsules in the Indian Ocean. The re-entry corridor within which landings might occur is 6000 km long and 100 km wide, stretching from Antarctica to India. To cover it will require 20 naval vessels, each with a helicopter, and 10 An-22 or Tu-95 long-range maritime reconnaissance and relay aircraft. Total cost: 600 million roubles. As Kamanin sees it, all this is due to Mishin's inability to design spacecraft capable of precision landing that also incorporates the landing and recovery aids requested by the VVS. Kamanin notes in his diary violent criticism of Mishin's disregard for the safety of the cosmonaut crews, development of crew-associated items at the last minute, unrealistic schedules and expectations, etc. etc. Severin reports that the lunar space suit he is designing will support the cosmonaut for three days, during walks extending 5 km. To do this requires a bulky suit weighing 100 kg. Kamanin disagrees, saying what is needed is to develop a simple and safe approach for the first landing, with a minimum programme for the cosmonaut - not the fantastic schemes of Mishin.
- 1969 January 29 - Lunar systems status - Program: Lunar L3, Lunar L1.
Review of spacesuit development at Zvezda Factory with Gay Severin. The specifications for the moon suit are 10 hours life, 80 kg mass, able to handle a heat load of 500 kcal/hour. But this load is insufficient for heavy work. By comparison, the suits used by Leonov and Khrunov could only handle 200-250 kcal/hour. 14 suits have been completed for tests. In the afternoon Soyuz descent systems are reviewed at Aleksander Lobanov's institute. The descent system parachutes are rated for a 10 tonne payload, but 40 tonnes of force are required to pull the parachute out of the compartment in the capsule. Individual parachutes could be provided for the crew, weight 6 kg each. This would evidently be considered as the back-up on L1 and LOK flights where the capsule had a side hatch and no reserve parachute.
- 1971 March 4 - N1/L3 Expert Commission - Program: Lunar L3. Launch Vehicle: N1, UR-700.
 | LK Egress Tests Another view of LK egress tests, showing the challenge of squeezing through the LK hatch in the Kretchet suit.... |
Pushkin and Kuznetsov brief Kamanin on the results of the N1/L3 expert commission. They found that the N1/L3 is unreliable and that the design needs to be fundamentally re-examined. Therefore the Soviet Ministers and Central Committee passed a decree that the commission must determine by 1 May 1971 what to do with the lunar project. Kamanin's opinion: abandon the N1-L3, modify Chelomei's UR-700 design to replace it, and design a new lunar landing spacecraft for missions in 1974-1975. Mishin is afraid of such a solution. Kamanin believes that the commission, headed by Keldysh, will finally recommend continued development and flight of Mishin's bad booster and even worse spacecraft. It is true that the N1 design has been substantially reworked in the last 18 months, but Kamanin believes it to be fundamentally flawed and that nothing can make it reliable. After Mishin pushed his Indian Ocean recovery plan for the L3, the VVS insisted on sea trials of the capsule. These showed the cosmonauts had to get out within 30 to 35 minutes before the valves to the interior started leaking seawater. The L3 is also unsafe due to the EVA method of transfer to the LK of a single unassisted cosmonaut. The Krechet spacesuit is very bulky and unmanoeuvrable. Prague wanted Gagarin's widow for International Women's Day.since Tereshkkova couldn't go, but she wants no part of public appearances.
Bibliography:- Kamanin, N P, Skritiy kosmos, Infortext, Moscow, 1995.
 | LK Egress Tests Another view of LK egress tests. This view makes clear the large size of the backpack of the Kretchet suit and the tight squeeze getting into and out of the LK lander.... Credit- Filin |
 | Early Egress Test Close-up of the earliest version of the Kretchet suit and LK mock-up during egress tests.... |
 | LK egress tests Numerous tests were conducted to determine the best hatch and ladder configuration for the cosmonaut in the bulky Kretchet spacesuit. It was found the standard Soyuz hatch had to be replaced by a customized oval hatch.... Credit- RKK Energia |
 | LK Interior Rare view of suited cosmonaut in the interior of the LK Interior during landing training. The cosmonaut had a viewing angle to the surface through the main window of 7 degrees from the vertical. A collimator indicated the predicted LK landing point.... Credit- RKK Energia |
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2008 except where otherwise noted.
|