This is what I have so far from a huge google trawl of the internet using Google Translate and cyrillic for the heavy long range interceptors of the various A-35/35M/135 systems:
А-350Ж / A-350Zh (ABM-1 GALOSH)
GRAU: 5В61 (5V61)
Interceptor Sustainer Motor: 5Д22 (5D22): 29,540 lbf single chamber liquid fuel motor using UDMH-NT.
Interceptor Steering Motor: 5Д18 (5D18) four chamber liquid fuel motor using UDMH-NT
Interceptor Length: 11.9 meters (calculated)
Interceptor Launch Mass: 15 tonnes
Booster Motor: Four clustered solid rocket boosters using ballistite; GRAU index 5С47 (5S47)
Booster Length: 7.9 meters
Booster Diameter: 2.57 meters
Booster Launch Mass: 15,000 kg
Overall Length: 19.8 meters
Overall Launch Mass: 32,700 kg
Maximum Range: 350 kilometers
Engagement Altitude: 120 kilometers
Transportation: Transported via MAZ-537s in sealed firing containers.
Notes: The 5D22 and 5D18 engines are actually the 15D13 and 15D14 engines on the UR-100 ICBM, but repackaged for use in the A-350 due to political reasons.
А-350Р / A-350R (ABM-1B GALOSH)
GRAU: 5В61Р (5V61R)
Interceptor Sustainer Motor: 5Д22 (5D22): 29,540 lbf single chamber liquid fuel motor using UDMH-NT.
Interceptor Steering Motor: 5Д18 (5D18) four chamber liquid fuel motor using UDMH-NT
Interceptor Length: 11.9 meters (calculated)
Interceptor Launch Mass: 15 tonnes
Booster Motor: Four clustered solid rocket boosters using ballistite; GRAU index 5С47 (5S47)
Booster Length: 7.9 meters
Booster Diameter: 2.57 meters
Booster Launch Mass: 15,000 kg
Overall Length: 19.8 meters
Overall Launch Mass: 32,700 kg
Minimum Range: 80 kilometers
Maximum Range: 520-640 kilometers
Minimum Engagement Altitude: 50 kilometers
Maximum Engagement Altitude: 350 kilometers
Transportation: Transported via MAZ-537s in sealed firing containers.
Notes: Modernized version of A-350Zh.
Emphasis placed on:
Redesigning guidance and navigation system to operate in wider regimes of exo/endo-atmospheric flight.
Developing radiation hardened autopilot and electronics to enable offensive sorting and to “juggle” multiple engagements at one time.
Greater 'useability' allowing faster reloads via significantly reducing the amount of time it took to fuel a missile, load the warhead and then emplace it on a launcher.
А-925 Азов / A-925 Azov (ABM-4 GORGON)
OKB: Факел / Fakel
GRAU: 51T6
IOC: December 1995
EOC: 2008
Interceptor Sustainer Motor: 5Д22 (5D22): 29,540 lbf single chamber liquid fuel motor using UDMH-NT.
Interceptor Steering Motor: 5Д18 (5D18) four chamber liquid fuel motor using UDMH-NT
Interceptor Length: 11.9 meters (calculated)
Interceptor Launch Mass: 15,000 kg
Booster Motor: Solid Rocket Booster
Booster Diameter: 2.57 meters
Booster Launch Mass: 30,000 kg
Total Launch Mass: 45,000 kg
Transportation: Transported via MAZ-547s in sealed firing containers.
Notes: Development of the A-925 began in December 1971, with the first launch occurring in March 1979. Full Scale Production seems to have occurred from 1990-1993. In February/March 2006 it was decided to remove these missiles from service; which was completed by 2008.