Skip to content
Molniya-M
EntityQ2155073· pop 11· linked from 549 articles

Also known as Molniya 8K78M

The Molniya-M (, GRAU index: 8K78M) was a Soviet and Russian launch vehicle derived from the R-7 Semyorka Intercontinental ballistic missile (ICBM).

Key facts

Rocket.image
Molniya-8K78M.svg
Rocket.caption
Drawing of the Molniya-M carrier rocket
Rocket.name
Molniya-M (R-7 8K78M)
Rocket.country origin
Soviet UnionRussia
Rocket.manufacturer
TsSKB-Progress
Rocket.function
Medium-lift launch vehicle
Rocket.height
43.4 m
Rocket.alt height
142.3 ft
Rocket.diameter
2.95 m
Rocket.alt diameter
9.67 ft
Rocket.mass
305,000 kg
Rocket.alt mass
672,000 lb
Rocket.stages
3
Rocket.family
R-7
Rocket.comparable
Soyuz-2/Fregat
Rocket.status
Retired
Rocket.sites
Baikonur, Sites 1/5 & 31/6
Rocket.launches
297

via Wikipedia infobox

Wikidata facts

Subclass of
R-7
Country of origin
Soviet Union
Image
Molniya-8K78M.svg
Sources (2)

via Wikidata · CC0

~6 min read

Encyclopedic overview

4 sections
Contents
  • Variants
  • Retirement
  • See also
  • References

The Molniya-M (, GRAU index: 8K78M) was a Soviet and Russian launch vehicle derived from the R-7 Semyorka Intercontinental ballistic missile (ICBM).

The original 8K78 booster had been the product of a rushed development program and its launch record was no better than the 8K72 Luna booster of 1958–1960. As 1962 ended, there had been 12 launches of 8K78s, ten of which failed (five Block L failures, four Block I failures, and one failure caused by the Block A core stage). left|thumb|Block L and 2MV planetary probe The two successful launches had had their probes (Venera 1 and Mars 1) fail en route to their respective planetary targets. As such, work began at the Korolev Bureau to improve the basic 8K78 vehicle. The core and strap-ons received the up-rated 8D74M engines and the Kosberg Bureau completely redesigned the Block I stage. The Block L engine was also slightly enhanced. The first six 8K78Ms built used RD-0108 engines in the Block I stage, which was also used in the two crewed Voskhod boosters, all subsequent 8K78Ms using RD-0110 engines which were shared with the Soyuz booster. Molniya boosters flown after the adaption of the new 11A511U core in 1973 used the improved 11D511 first stage engines. While 11A511U cores flown on other R-7 vehicles switched to a shorter instrument packet, the Molniya continued using the old "long" instrument packet.

Excerpted from Wikipedia’s “Molniya-M” article, available under the CC BY-SA 4.0 licence.

Gallery (2)