It was decided that henceforth, cosmonauts would wear pressure suits for launch and the return to Earth. Also, a system was installed to automatically pump air into the descent module in the event of decompression. Additionally, the ventilation valves were modified so a premature opening would cause them to re-close automatically. Of course these changes meant the spacecraft could only accommodate two cosmonauts.
Finally, on the morning of February 21, all the population of the N1 assembly area and a residential area, situated just south of the launch pad, was ordered to evacuate. The giant service structure then rolled away leaving the dark-gray rocket with a white payload fairing towering under sunny skies. The weather was extremely cold, with temperatures falling to minus 44 C degrees, and stormy winds. In the fortified firing control room, the Commander of the 6th Directorate, took the firing command position at the main periscope…
Apollo CSM/LM vs. Soviet L3 Complex. Credit Mark Wade
N1 image taken by US KH-8 Reconnaissance satellite
On August the third 1964 Decree number 655-268 was issued by the Central Committee of the Communist Party. For the first time a command was given for OKB-1 to put one man on the moon and return him safely to earth before the United States (Keep in mind the US already had already begun their Lunar program more than three years earlier, in April 1961).
N1-L3 as per advanced project, 1964. Credit Astronautix
The L-3 manned spacecraft was designed to make a direct lunar landing using the earth orbit rendezvous method. It was a 200 metric ton spacecraft requiring three N1 launches and a single Soyuz 11A5ll launch to assemble in low earth orbit. The first N1 launch would place the 75 metric ton partially-fueled Trans Lunar Injection stage and L3 spacecraft into low earth orbit. Two further N1 launches would orbit 75 metric ton tankers which would rendezvous and dock with the first payload and top off its propellant tanks. Then the Soyuz would be launched for an automated rear-end docking with the entire L3 stack.
Comparison of U.S. Saturn V with Soviet N1/L3
N-1 draft project design of 1962. credit Astronautix
Trouble began on the sixth day of the flight, November 17. The capsule developed an atmospheric leak, the pressure first dropping from 760 to 380 mm of Mercury. With the drop in cabin pressure all the animal test subjects died. It would have killed any Cosmonaut not wearing a spacesuit.