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Nadiradze, Aleksandr Davidovich
Nadiradze
Nadiradze
Russian chief designer. Director and Chief Designer of the Moscow Institute for Thermal Technology 1961-1987. Pioneering developer of Soviet solid propellant missiles.

AKA: Moscow Heat Engineering Institute; Moscow Institute of Thermal Technology; NII-TT. Born: 1914. Died: 1987-01-01.

Country: Russia. Launch Vehicles: R-65, Frog 8, Frog 9, Temp-S.2M, RT-20, RT-21, R-75, R-70, 9K76, RT-22, Temp-S, 15Zh45, Temp-2S, Pioner, 9K714B, 15Zh53, Topol', Pioner UTTKh, 9K76B, Skorost, Start-1, Topol'-M, Start, Start-1.2, Bulava, RS-24. Stages: RD RT-21-3, RD RT-21 (1), RD RT-21-2, 15Zh58A, 15Zh58B, 15Zh58V, DS engine, MIHT-1, MIHT-2, MIHT-3, MIHT-4. More at: 5817. Bibliography: 475.



1968 January 23 - .
1968 December 23 - . LV Family: N1. Launch Vehicle: N1.
1969 May 29 - .
  • N1 State Commission - . Nation: Russia. Related Persons: Afanasyev, Sergei, Barmin, Bushuyev, Chelomei, Keldysh, Mishin, Nadiradze, Okhapkin, Pashkov, Smirnov, Tyulin, Yangel. Program: Lunar L3. Spacecraft: Aelita satellite, LK, Soyuz 7K-L1A, Soyuz 7K-LOK.

    Over two days a State Commission reviewed all of the conclusions of the N1 3L failure investigation and the readiness of N1 5L for flight. All of the fixes identified to remedy the 3L failure had been incorporated into 5L. It was felt that the behaviour of the systems in fire conditions were understood and appropriate measures had been taken. The wiring had been rerouted and insulated. Barmin wanted the system not to shut down any engines under any conditions during the first 15-20 seconds of flight, so that the booster would clear the pad and there would be no risk of the pad's destruction. But there was no time to develop such measures before the 5L launch; it could only be added in vehicle 6L. Additional Details: here....



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