By 1992 Buran was now out of the picture and the plan was reduced in scale again. These revised plans were approved by the Council of Chief Designers on 24 November 1992. Mir-2 returned to its original planned 65 degree orbit, and would be assembled and flown separately from Mir. It would now consist of the DOS-8 core module, and a cross beam called the NEP (scientific-energy platform). This was equipped with equipment already proven on Mir: MSB retractable solar panels, Sfora thruster packages, small scientific packages as demonstrated on Kvant.
The add-on modules now used the Progress-M service module as a tug, and were reduced in size for launch by either the Soyuz or Zenit launch vehicles. Earth resources had been eliminated as a station activity (presumably Mir work had shown photographing the earth was more practical using free-flying satellites). Instead the four modules would weigh only 3 to 4 metric tons each and consist of:
- Docking Module - with the APDS universal androgynous docking system, and a side hatch for space walks
- Resource Module - Equipped with gyrodynes for orienting the station and a passive docking port for docking of Soyuz or Progress ferry spacecraft
- Technology Module - with materials experiments
- Biotechnology Module
A more capable resupply craft could be realized by using the Progress module with larger cargo or space station modules. The planned Progress-M2 11F615A75 was originally designed for use with the 90 metric ton module Mir-2. Redesigned in 1992-1993 for use with the more modest Mir-2 it had a revised index number of 11F615A77. The 13.3 metric ton, 12.6 m long vehicle consisted of the 5.3 metric ton service module, a 2.3 metric ton pressurized forward module equipped with a docking port, and could hold 5.7 metric tons of cargo. It could also be outfitted as a laboratory and left docked with the Mir-2.