Luna E-6 No.2
| Mission type | Lunar lander |
|---|---|
| COSPAR ID | 1963-001B |
| SATCAT no. | 522 |
| Mission duration | Launch failure |
| Spacecraft properties | |
| Manufacturer | OKB-1 |
| Launch mass | 1,500 kilograms (3,300 lb) |
| Start of mission | |
| Launch date | 4 January 1963, 08:49 UTC |
| Rocket | Molniya-L 8K78L s/n T103-09 |
| Launch site | Baikonur 1/5 |
| End of mission | |
| Decay date | 11 January 1963 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime |
Low Earth (achieved) Heliocentric (intended) |
| Perigee | 178 kilometres (111 mi) |
| Apogee | 194 kilometres (121 mi) |
| Inclination | 64.7 degrees |
| Period | 88.21 minutes |
Luna E-6 No.2, also identified as No.1, and sometimes known in the West as Sputnik 25, was a Soviet spacecraft which launched in 1963, but was placed into a useless orbit due to a problem with the upper stage of the rocket that launched it. It was a 1,500-kilogram (3,300 lb) Luna E-6 spacecraft, the first of twelve to be launched, It was intended to be the first spacecraft to perform a soft landing on the Moon, a goal which would eventually be accomplished by the final E-6 spacecraft, Luna 9.
Luna E-6 No.2 was launched at 08:49 UTC on 4 January 1963, atop a Molniya-L 8K78L carrier rocket, flying from Site 1/5 at the Baikonur Cosmodrome. The lower stages of the rocket performed nominally, delivering the upper stage and payload into low Earth orbit, however a transformer in the upper stage malfunctioned, which resulted in its ullage motors failing to ignite when the stage began its start-up sequence, sixty six minutes after launch. It remained in low Earth orbit until it decayed on 11 January 1963. It was the first spacecraft to be launched in 1963, and consequently the first to be assigned an International Designator, under the new system which had been introduced at the start of the year.
The spacecraft consisted of a cylindrical section containing rockets and fuel for manoeuvring, attitude control and landing, as well as radio transmitters, and a 100-kilogram (220 lb) instrumented probe, which would have been ejected onto the surface after the spacecraft landed, carrying a camera and devices to measure radiation. It was intended to return data on the mechanical characteristics of the lunar surface, the hazards presented by the topology such as craters, rocks, and other obstructions, and radiation, in preparation for future manned landings.
The designations Sputnik 33, and later Sputnik 25 were used by the United States Naval Space Command to identify the spacecraft in its Satellite Situation Summary documents, since the Soviet Union did not release the internal designations of its spacecraft at that time, and had not assigned it an official name due to its failure to depart geocentric orbit.
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