TMK: Difference between revisions

For other uses, see TMK (disambiguation).

Artist's depiction of TMK-MAVR on a Venus flyby

TMK (Template:Lang-ru) was the designation of a Soviet space exploration project to send a manned flight to Mars and Venus (TMK-MAVR design) without landing.

The TMK-1 spacecraft was due to be launched in 1971 and make a three-year-long flight including a Mars flyby, at which time probes would have been dropped. Expanded project variations, such as the TMK-E, Mavr or KK, including a Venus flyby, electric propulsion or a manned Mars landing were also proposed.

The TMK project was planned as an answer from the Soviet Union to the United States' manned Moon landings. A previous Martian Piloted Complex mission was proposed in 1956. The project was never completed because the required N1 rocket never flew successfully.

TMK-1

TMK-1

Mission type	Manned interplanetary
Mission duration	1095 days
Spacecraft properties
Spacecraft type	RP-1/LOX
Dimensions	Length: 39 feet (12 m) Diameter: 19.60 feet (5.97 m) Volume: 4,555.6 cubic feet (129.00 m3)
Crew
Crew size	3
Members	Soviet cosmonauts
Start of mission
Launch date	June 8, 1971 (1971-06-08) (planned)
Rocket	N1
End of mission
Landing date	July 10, 1974 (1974-07-10) (planned)
Flyby of Mars
Closest approach	April 1972 (planned)

The first flight to Mars of the TMK-1 was planned to begin on June 8, 1971.

The 75 metric ton TMK-1 spacecraft would take a crew of three on a Mars flyby mission. After a 10½ month flight the crew would race past Mars, dropping remote-controlled landers, and then be flung into an Earth-return trajectory. Earth return would happen on July 10, 1974, after a voyage of three years, one month, and two days.

Spacecraft configuration:

• A habitation or pilot compartment, with an internal volume of 25 cubic meters
• A work or equipment section, including the hatch for extra-vehicular activities and a solar storm shelter should solar flares increase radiation to dangerous levels. Total volume of the section would be 25 cubic meters.
• A biological systems compartment, with the SOZh closed-cycle environmental control system, with a total volume of 75 cubic meters
• An aggregate section, with the Mars probe capsules, the KDU midcourse correction engine, the SOZh solar concentrator and solar panels, and radio antennas
• The SA crew Earth reentry capsule, about 4 m in diameter

TMK-E

TMK-E

Mission type	Manned interplanetary
Mission duration	1096 days
Spacecraft properties
Spacecraft type	Nuclear electric (Xenon) Thrust: 74 newtons (17 lbf)
Dimensions	Length: 574 feet (175 m) Diameter: 19.60 feet (5.97 m)
Crew
Crew size	6
Members	Soviet cosmonauts
Start of mission
Rocket	N1
Mars lander

This variation was proposed in 1960, and consisted of a complete Mars landing expedition to be assembled in Earth orbit using several N1 launches. The spacecraft would be powered by nuclear electric engines and five landers would deliver a nuclear-powered Mars Train on the surface for a one-year mission.

The TMK-E would be capable of a three-year flight to Mars and return, of which one year was powered flight. It would measure 175 m in length and house a crew of six. Six landing craft were included, two for the crew and four for the Mars Train vehicles.

Mavr (MArs - VeneRa)

MAVR

Mission type	Manned interplanetary
Mission duration	680 days
Spacecraft properties
Spacecraft type	RP-1/LOX
Dimensions	Length: 82 feet (25 m) Diameter: 19.60 feet (5.97 m) Volume: 45.0 cubic metres (1,590 cu ft)
Crew
Crew size	3
Members	Soviet cosmonauts
Start of mission
Rocket	N1
Flyby of Mars
Flyby of Venus

A variation of the TMK mission planning involved a flyby of Venus on the return voyage, and was given the code name "Mavr" (MArs - VeneRa), meaning Mars - Venus.

KK - Space Complex for Delivering a Piloted Expedition to Mars

KK - Space Complex for Delivering a Piloted Expedition to Mars
Description
Role:	Mars Expedition
Crew:	three
Rocket engines
Main Engine (Xenon) :	14 lbf ea	61 N
Performance
Endurance:	630 days	30 days Mars stay

In 1966, a final version of the TMK studies was known as KK - Space Complex for Delivering a Piloted Expedition to Mars. Nuclear electric propulsion was to be used for the 630-day mission. The craft structure consisted of:

• EK - Expeditionary spacecraft: command center for piloting in interplanetary space
• OK - Orbital Complex: living and work compartments and the life support systems
• SA - The Landing Module, AV - The Ascent Module and RV - The Ascent Rocket stage
• PS - The Planetary Station: used by the expedition on the Martian surface for life support and scientific research

The launch was planned for 1980, with a crew of three cosmonauts. Mars stay duration would be 30 days.

Mission data:

• Total Payload Required in Low Earth Orbit-metric tons: 150
• Total Propellant Required-metric tons: 24
• Number of Launches Required to Assemble Payload in Low Earth Orbit: 2
• Launch Vehicle: N1

See also

• Manned mission to Mars
• Manned Venus Flyby

External links

• Anatoly Zak's TMK page
• TMK page on astronautix
• TMK-MAVR page on astronautix