Soyuz Kontakt A
Provisional drawing of Soyuz Kontakt A (Active) derivative of Soyuz for earth orbit tests of Kontakt lunar orbit docking system. It is uncertain if the Soyuz included the forward-mounted manoeuvring engines, or just the active docking mechanism of the LOK lunar orbiter. Certainly the LOK's cupola forward viewing port would have to be included in the orbital module.
Credit: © Mark Wade
AKA: 11F615. Status: Cancelled 1974. Thrust: 4.09 kN (919 lbf). Gross mass: 6,560 kg (14,460 lb). Unfuelled mass: 6,060 kg (13,360 lb). Specific impulse: 282 s. Height: 7.95 m (26.08 ft). Span: 9.80 m (32.10 ft).
Kontakt was developed for the lunar orbit rendezvous of the 7K-OK manned lunar orbiter and LK lunar lander. It utilized a hexagonal grid on the passive craft and a three-pronged grappler on the active spacecraft to allow a soft docking between the two spacecraft. The Kontakt system used manual optical methods for rendezvous and docking rather than the heavier automatic Igla radar system mounted on the 7K-OK. No hard docking was possible and crew transfer was by extravehicular activity.
The 7K-OK adaptation would have involved launch of two Soyuz by 11A511 boosters, with rendezvous and crew transfer in earth orbit. Crews were trained for these tests but due to delays and final cancellation of the N1-L3 lunar orbit rendezvous mission, the spacecraft never flew.
Crew Size: 3. Orbital Storage: 35 days. Habitable Volume: 9.00 m3. Spacecraft delta v: 390 m/s (1,270 ft/sec). Electric System: 0.50 average kW.
|Soyuz Kontakt P|
Provisional drawing of Soyuz Kontakt P (Passive) derivative of Soyuz for earth orbit tests of Kontakt lunar orbit docking system. It is uncertain if the Soyuz included the forward-mounted manoeuvring engines, or just the passive docking mechanism of the LK lunar lander. Certainly the LK's forward viewing port and docking optical device would have to be included in the orbital module. It is not known if the downward-looking viewport and extensive scallop of the LK cabin was a feature.
Credit: © Mark Wade
|Kontakt Docking Mech|
Kontact docking grappler. The three arms at the bottom faced outward from the docking assembly. MAI, March 1994
Credit: © Dietrich Haeseler
Acting director Mishin held a brainstorming session with this top managers to address "...our inconsistent lunar program". He noted then-current contradictory approaches: 1. Return to a two-launch scheme (podsadka, as baseline); 2. Keep with direct landing; 3. Use a Block D with storable propellants; 4. Use the 7K-OK as the designated return spacecraft. He noted that the L1 program was a diversion for the bureau to the core objective of landing a cosmonaut on the moon (the L3 program). Among the advantages of continuing with the L1, he noted that it "Utilizes the 7K-OK" - evidently there was no purpose for the spacecraft beyond the L1 mission in the podsadka scenario. He asks for frank opinions from his managers. V Rauschenbach noted that they "..have to do the L-1 … and therefore we will have to use a 2-launch scheme based on the L1-S". BE Chertok: discussed the rendezvous and docking systems for the various spacecraft: L1-S - "Igla"; LOK - "Kontakt" (since "Igla" cannot be used on the LOK (due to mass considerations); or a new system for the LOK. (Mishin Diaries 1-226) Here we have an indication that the L1 podsadka version did use the Igla system, which makes complete sense, since the Soyuz 7K-OK missions conducted dress rehearsals for podsadka using this system to rendezvous and dock two 7K-OK spacecraft in earth orbit.
Chertok compared the "Kontakt" and "Liga" systems, and noted that the "Liga" elements in the control loop control system simplified LK landing. MS Ryazanskiy noted that this contradicted a decision two years ago to have the LK make an autonomous landing on the moon (LK homing on and landing near a beacon was postponed at that time). But AS Mnatsanakyan supported the approach, saying it was necessary to speed up the development of the "Liga"; it provided a precision landing on the moon within 50 to 100 m of the target. (Mishin Diaries 2-120).
The commission considers plans for the rest of the Soyuz production. Spacecraft s/n 14, 15, and 16 are to fly in August 1969, 17 and 18 in November 1969, and 19 and 20 in February-March 1970. Crews selected for the August flights are: for spacecraft 14, Shonin and Kubasov; for 15, Filipchenko, Volkov, and Gorbatko; for 16, Nikolayev and Sevastyanov. Back-ups will be Kuklin, Grechko, and Kolodin. All of the spacecraft will fly 4 to 5 day missions. Spacecraft 15 and 16 will dock and remain together 2 or 3 days to form an 'orbital station'. Experiments planned for the flight are:
Spacecraft 17 through 20 will fly 15 to 16 day missions to demonstrate the new SZhO life support system for the L3, and conduct rendezvous and docking operations using the L3's Kontakt system. Additional Details: here....
The Kontakt system designed for the lunar orbit rendezvous and docking of the LOK lunar orbiter and LK lunar lander was to be mounted on two Soyuz spacecraft and tested in earth orbit. These flights were continuously delayed after the success of Apollo 11 and finally cancelled.
It was originally planned to fly two Soyuz spacecraft in August-September 1970, but at the end of December it was ordered that this be changed to a single 20 day flight in April 1970. Kamanin was given only two days to put together a training programme that had to prepare the cosmonauts for flight by 20 March. The State Commission meets and decides to move the Soyuz 9 flight to May, even though Kamanin says he can support the April schedule. It is the scientific institutes who say they cannot finish development of their experiments - even to meet the May schedule. Kamanin blames such chaos on Smirnov, Serbin, and Ustinov.
Meeting with Mishin. It is clear that he wanted to continue with the original plan for a dual Soyuz flight in August. It was Afanasyev and Kerimov who were pushing for a single long-duration flight in May. There is no action by the Ministry of Defence to provide rational decision making in regard to manned spaceflight.
A meeting is held on the DOS project. The Central Committee and Soviet Ministers have directed that two DOS space stations be completed by the end of 1970. TsNIIMASH thinks this is impossible - the task can be accomplished in no less than 18 to 24 months. Mishin insists it can be done in ten months, as directed. Kamanin believes he won't even have it ready by the second half of 1971. It took five to seven years to just bring the Almaz, Soyuz VI, and L1 to flight status. This DOS will stop work on all other projects. Mishin still wants to fly two Soyuz spacecraft to test Bogomolov's Kontakt docking system for the L3.
The training plan for DOS#1 is reviewed. The station is to be launched by February 1971. Soyuz 10 and Soyuz 11 will dock with it and crew the station for two to three months, according to Mishin's plan. This however will slow down flight test of Bogomolov's Kontakt docking system for the L3. This was to have been ready by January 1970, but it is still not ready for flight. On the other hand, the completion of the DOS station within four to five months is not possible. There are currently 12 cosmonauts in training for DOS, and ten for Soyuz flights. Popovich heads a group of 22 cosmonauts training for Almaz; and Bykovsky heads a group on lunar issues. The new trainers and simulators are on schedule; the existing ones are being heavily used.
Crews are formed for six Soyuz (Kontakt?) flights. Soyuz s/n 18 - Filipchenko and Grechko; Soyuz s/n 19 - Lazarev and Makarov; Soyuz s/n 20 - Vorobyov and Yazdovsky; Soyuz s/n 21 - Yakovlelv and Porvatkin; Soyuz s/n 22 - Kovalyonok and Isakov; Soyuz s/n 23 - Shcheglov and [illegible]. Five crews are training for Salyut flights: Crew 1, Leonov, Rukavishnikov, and Kolodin; Crew 2, Gubarev, Sevastyanov, and Voronov. TsKBEM engineer cosmonauts are to be selected will round out the last three crews, but VVS members will be: Crew 3, Klimuk, Artyukhin; Crew 4, Bykovskyy, Alekseyev; Crew 5, Gorbatko. Leonov and Gubarev will have their crews fully ready for Soyuz 12 by 30 June, for a launch date between 15-20 July. Leonov is asking to go to East Germany for two to three days in the first week of July. Kamanin is fully opposed to this - he is thinkng not of his upcoming flight, but the exhibition of his paintings at the Prezdensk Gallery!
The reason for continuing with development of the L3 Kontakt docking system even after the L3 was cancelled was that it was to be used in MKBS. The note reads: Chertok - 7K-OK number 18 - rework using the propulsion system from number 36. Work on "Kontakt" to continue, as it can be used in the MKBS).
"1. Klyucharev VM: Omsk plant (Director Kolupaev) - Delayed production of 7KS living compartments. ZEM - develop work and schedules to recover schedule for completion of 7KS modules. 2. Chertok: 7K-OK number 18 - rework using the proulsion system from number 36. Work on "Kontakt" to continue, as it can be used in the MKBS'.