Luna (rocket)

Luna 8K72
	Blok E upper stage, with Luna payload
Function	Carrier rocket
Manufacturer	RKK Energia
Country of origin	Soviet Union
Size
Mass	277,000 kg (611,000 lb)
Stages	3
Capacity
Payload to LEO	4,000 kilograms (8,800 lb)
Associated rockets
Family	R-7
Launch history
Status	Retired
Launch sites	Baikonur: LC-1/5
Total launches	9
Successes	3
Notable payloads	Luna probes
First stage (Block B, V, G, D)
Engines	1 RD-107-8D74-1958
Thrust	990.00 kN
Burn time	120 seconds
Fuel	Kerosene/LOX
Second stage (Block A)
Engines	1 RD-108-8D75-1958
Thrust	936.500 kN
Burn time	320 seconds
Fuel	RP-1/LOX
Third stage (Block E)
Engines	1 RD-0105
Thrust	49.0 kN
Burn time	316 seconds
Fuel	Kerosene/LOX

Short description: Model of carrier rocket

The Luna 8K72 vehicles were carrier rockets used by the Soviet Union for nine space probe launch attempts in the Luna programme between 23 September 1958 and 16 April 1960.^[1] Like many other Soviet launchers of that era, the Luna 8K72 vehicles were derived from the R-7 Semyorka design, part of the R-7 (rocket family), which was also the basis for the Vostok and modern Soyuz rocket.

Launches

Luna 8K72 was launched nine times from Baikonur LC-1/5:^[2]

Launch Date	Serial No.	LS	Payload	Result
23.09.1958	B1-3	Ba LC-1/5	Luna E-1 No.1	Failure
11.10.1958	B1-4	Ba LC-1/5	Luna E-1 No.2	Failure
04.12.1958	B1-5	Ba LC-1/5	Luna E-1 No.3	Failure
02.01.1959	B1-6	Ba LC-1/5	Luna 1	Success
18.06.1959	I1-7	Ba LC-1/5	Luna E-1A No.1	Failure
12.09.1959	I1-7B	Ba LC-1/5	Luna 2	Success
04.10.1959	I1-8	Ba LC-1/5	Luna 3	Success
15.04.1960	L1-9	Ba LC-1/5	Luna E-3 No.1	Partial Success
16.04.1960	L1-9A	Ba LC-1/5	Luna E-3 No.2	Failure

The first flight of a Luna 8K72 (September 1958), which was to launch the Luna E-1 No.1 probe, ended 92 seconds after launch when the rocket broke up from longitudinal ("pogo") oscillations, causing the strap-ons to separate from the vehicle, which then crashed downrange.^[3]

The second flight of a Luna 8K72 (October 1958), which was to launch the Luna E-1 No.2 probe, ended 104 seconds after launch when the rocket again disintegrated from vibration.

The third flight of a Luna 8K72 (December 1958), which was to launch the Luna E-1 No.3 probe, ended 245 seconds after launch when the Blok A core stage shut down from loss of engine lubricant.

The resonant vibration problem suffered by the 8K72 booster was the cause of a major argument between the Korolev and Glushko design bureaus. It was believed that the vibrations developed as a consequence of adding the Blok E upper stage to the R-7, shifting its center of mass.

The first probe launched by a Luna 8K72 to reach orbit was Luna 1, launched on 2 January 1959, which was intended as a lunar impactor mission.^[4] Luna 1 instead passed within 5,995 kilometres (3,725 mi) of the Moon's surface 4 January 1959, and then went into orbit around the Sun between the orbits of Earth and Mars.^[5]

The fifth flight of a Luna 8K72 (18 June 1959), which was to launch the Luna E-1A No.1 probe, ended 153 seconds after launch due to a guidance malfunction of the Blok A core stage, leading to engine shutdown.^[6]

Luna 2 was launched by a Luna 8K72 on 12 September 1959. It was the first spacecraft to impact the lunar surface.

The final successful launch of a Luna 8K72 took place on 4 October 1959. The Luna 3 spacecraft took the first photographs of the far side of the Moon.

The eighth flight of a Luna 8K72 (March 1960), which was to launch the Luna E-3 No.1 probe, ended 435 seconds after launch when the Blok E upper stage developed insufficient thrust, causing the Luna probe to reenter the atmosphere and burn up.

The ninth flight of a Luna 8K72 (April 1960), which was to launch the Luna E-3 No.2 probe, failed when the Blok G strap-on booster developed only 75% thrust at liftoff, breaking away from the launch vehicle, which then disintegrated, the strap-ons flying in random directions and exploding as they impacted the ground. The Blok A core stage then crashed into a salt lake.

References

↑ "Soyuz - Version: Luna 8K72". Encyclopedia Astronautica. http://www.astronautix.com/lvs/soyuz.htm.
↑ "Vostok-L (8K72)" (in en). https://space.skyrocket.de/doc_lau_det/vostok-l.htm.
↑ "Tentatively Identified Missions and Launch Failures". NASA NSSDC. 2005-01-06. http://nssdc.gsfc.nasa.gov/planetary/tent_launch.html.
↑ "Soyuz - Soyuz Chronology". Encyclopedia Astronautica. http://www.astronautix.com/lvs/soyuz.htm.
↑ "Luna 1 - NSSDC ID: 1959-012A". NASA. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1959-012A.
↑ Reichl, Eugen (2017). Moskaus Mondprogramm. Paul Pietsch Verlage GmbH & Co (1. Auflage ed.). Stuttgart. ISBN 978-3-613-04027-4. OCLC 987572365. https://www.worldcat.org/oclc/987572365.

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Original source: https://en.wikipedia.org/wiki/Luna (rocket). Read more

[1] "Soyuz - Version: Luna 8K72". Encyclopedia Astronautica. http://www.astronautix.com/lvs/soyuz.htm.

[2] "Vostok-L (8K72)" (in en). https://space.skyrocket.de/doc_lau_det/vostok-l.htm.

[tent-3] "Tentatively Identified Missions and Launch Failures". NASA NSSDC. 2005-01-06. http://nssdc.gsfc.nasa.gov/planetary/tent_launch.html.

[4] "Soyuz - Soyuz Chronology". Encyclopedia Astronautica. http://www.astronautix.com/lvs/soyuz.htm.

[5] "Luna 1 - NSSDC ID: 1959-012A". NASA. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1959-012A.

[6] Reichl, Eugen (2017). Moskaus Mondprogramm. Paul Pietsch Verlage GmbH & Co (1. Auflage ed.). Stuttgart. ISBN 978-3-613-04027-4. OCLC 987572365. https://www.worldcat.org/oclc/987572365.

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v t e Soviet, Russian, and Ukrainian launch vehicles
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Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
Symbol ^† indicates projects terminated before a successful orbital launch

Luna (rocket)

Topic: Engineering

Launches

References