 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 toLEO | |
| Mass | 4,000 kilograms (8,800 lb) |
| Associated rockets | |
| Family | R-7 |
| Launch history | |
| Status | Retired |
| Launch sites | Baikonur:LC-1/5 |
| Total launches | 9 |
| Success(es) | 3 |
| Carries passengers or cargo | Luna probes |
| First stage – Block B, V, G, D | |
| Powered by | 1RD-107-8D74-1958 |
| Maximum thrust | 990.00 kN |
| Burn time | 120 seconds |
| Propellant | Kerosene/LOX |
| Second stage – Block A | |
| Powered by | 1RD-108-8D75-1958 |
| Maximum thrust | 936.500 kN |
| Burn time | 320 seconds |
| Propellant | RP-1/LOX |
| Third stage – Block E | |
| Powered by | 1RD-0105 |
| Maximum thrust | 49.0 kN |
| Burn time | 316 seconds |
| Propellant | Kerosene/LOX |
TheLuna 8K72 vehicles werecarrier rockets used by theSoviet Union for ninespace probe launch attempts in theLuna 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 theR-7 Semyorka design, part of theR-7 rocket family, which was also the basis for theVostok and modernSoyuz rockets.
The 8K72 was the first R-7 variant explicitly designed as a carrier rocket and it incorporated a few features that became standard on all later R-7 carrier rockets including thicker tank walls to support the weight of upper stages and the AVD malfunction detection system, which wouldterminate engine thrust if the booster's operating parameters (engine performance, electrical power, or flight trajectory) deviated from normal.
Luna 8K72 was launched nine times fromBaikonur 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 theLuna 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 theLuna 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 theLuna E-1 No.3 probe, ended 245 seconds after launch when the Blok A core stage shut down from loss of engine lubricant.
Theresonant 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 itscenter of mass.
The first probe launched by a Luna 8K72 to reach orbit wasLuna 1, launched on 2 January 1959, which was intended as a lunarimpactor 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 theLuna 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. TheLuna 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 theLuna 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 theLuna 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.
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