ABM-1 Galosh
| A-350 | |
|---|---|
Operational range | 320–350 km |
| Flight ceiling | 120 km exosphere |
| Flight altitude | unknown |
| Maximum speed | Mach 4 |
Guidance system | Radar Command guidance |
Launch platform | A-35 Aldan[3] |
The A-350
.The A-350 was introduced during the 1960s with mechanically steered
The A-350R (NATO reporting name ABM-1B) was introduced with the advanced A-35M missile system and became operational during 1978. This system was tested at the Sary Shagan Launch Facility with five test flights during 1971, 1976, and 1977, with two more tests during 1993 and 1999.[8]
The next generation of missiles, introduced with the
Design
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The A-350 was a three-stage solid-fueled design with a range of over 300 kilometers. It was improved with a restartable liquid-fueled third stage. This gave a much improved post-launch and re-targeting capabilities. The A-350 are launched from above-ground launchers. [9]
The missile design was done by
The system had multiple radars during the different phases including the Don-2N radar and Dnestr radar early warning systems, and the Dunay radar target acquisition systems. The A-35 with radar was designed by Chief Designer K. B. Kisunko.[7]
Radar systems
The idea for this system was to protect Moscow from nuclear attack by the United States. The Russian government began studies during 1958 with preliminary designs from General Designer K. B. Kisunko. Further designs and development were moved to TsNPO Vympel. Radar systems were tested with Duna-3 single direction search radar and the
Missile warhead
The A-350 developed through a period of growth and modifications. Configurations included an improved A-350Zh with tests during 1973. Eventually, the design changed again with radiation-hardened cases and became the A-350R for Phase 2 deployment in 1974.
Construction
The construction of the A-35 system began during 1962 with 16 primary sites including command post, radar installations and firing complexes for 8–16 missile launchers. Some of the existing sites of the old
.One of the
The construction plan changed a number of times, varying the locations, sectors or quadrants, and number of launchers. The system finalized at 8 sites with total of 64 launchers, with 4 major radar centers completed.[9]
Advanced A-35M system (ABM-1B)
With on-going advancements in the ABM system, radars, missile and warheads, the evolution of the A-35 became the A-35M. The "M" for modernization, was brought on through the advanced developments at 10 different Russian institutes. One primary upgrade was in the Dunay-3U radar systems enhanced with a dedicated sector search functionality. Along with other upgrades, actual air tests were performed with different configurations between 1976 and 1977. Phase 3 of the A-35M went on-line in 1978.[7]
See also
- Treaties
- Related US missiles
- Nike Zeus
- Sprint (missile)
- LIM-49A Spartan
References
- ^ Astronautix: 5S47 Solid Rocket Motor Archived 11 November 2011 at the Wayback Machine Accessed: 29 Dec 2011
- ^ Astronautix: 5D22 Solid Rocket Motor Archived 11 November 2011 at the Wayback Machine Accessed: 29 Dec 2011
- ^ astronautix.com: A-35 Archived 11 November 2011 at the Wayback Machine Accessed: 29 Dec 2011
- ^ "Some important Soviet solid fuel missiles". www.b14643.de.
- ^ a b "NATO Designation-systems Index: Soviet Anti-ballistic Missiles (ABM)". Retrieved 14 November 2014.
- ^ Wonderland.org: ABM-1 Archived 9 February 2008 at the Wayback Machine
- ^ a b c d "A-35". Encyclopedia Astronautica. Archived from the original on 18 July 2008. Retrieved 25 August 2008.
- ^ "Astronautix: Sary Shagan". Archived from the original on 27 December 2016. Retrieved 26 October 2020.
- ^ a b "Federation of Scientists: ABM-1". Retrieved 14 November 2014.
- Notes
External links
- Secret Projects: Russian ABM system
- AeroSpaceWEb: ABMs
- ABM-1 Galosh and A-35 site photos Archived 11 August 2007 at the Wayback Machine scroll down
- NATO Soviet Naming Conventions for ABMs
- FAS.org: ABM-2