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1Nosach LM, 1Povnitsa OYu., 1Zhovnovata VL. Adenoviruses as a model in the study of the effect of space flight factors. Kosm. nauka tehnol. 2007 ;13(2):086-089.
1Nokel VP, 1Nikolaenko VM, 1Yampolsky Yu.S, 1Yerimichoy IN, 2Bezrukih VV, 1Venediktov Yu.I, 1Chemes EA, 1Mamedov KYa. Investigation of the efficiency of processing algorithms for symmetric dual Langmuir probe (SDLS) based on the proposed quality indicator. Kosm. nauka tehnol. 2002 ;8(Supplement2):213-219.
1Nokel VP, 1Nikolaenko VM, 1Yampolsky Yu.S, 1Mamedov KYa., 1Venediktov Yu.I, 2Shuvalov VA, 3Dovgal SG, 4Gdalevich GL. Measuring system for direct determination of plasma parameters based on a symmetric dual Langmuir probe (SDLC). Kosm. nauka tehnol. 2002 ;8(Supplement2):207-212.
1Nikolin SO, 1Sokol GI. The influence of gas-dynamic processes on acoustic radiation in the interaction of impinging jet with the flat plate. Space Science and Technology. 2020 ;26(3):20-31.
1Nikolenko IV, 1Neyachenko DI, 1Zenkovich AD, 2Smirnov MA, 2Kryuchkov SV, 2Drums SI. Search and observations of celestial bodies in near-Earth space on the telescope «ZEIS-1000» in the CJSC. Kosm. nauka tehnol. 2002 ;8(Supplement2):312-317.
1Nikolenko EYu., 1Skrypnyk OP. Measurement of final geometrical parameters for space devices boosters. Kosm. nauka tehnol. 2001 ;7(Supplement1):058-060.
1Nihreieva OO. The international legal regime of outer space between Res Communis and Res Nullius. Space Science and Technology. 2022 ;28(1):23-42.
1Nevodovsky EP, 1Vidmachenko AP, 1Morozhenko OV, 1Nevodovsky PV, 1Syniavskyi II. The Ukrainian Youth Satellite: investigation of the Earth's aerosol stratum with the use of UV-polarimeter. Kosm. nauka tehnol. 2004 ;10(5-6):027-031.
1Nesterenko GV, 2Shelkovenkov DA, 1Ivanova EA, 1Bondar EYu. On the possibility of provision of autonomous high-accuracy synchronization of time scales (frequency) of space-apart keepers on the basis of external source signals. Kosm. nauka tehnol. 2007 ;13(Supplement1):078-079 .
Nerus MA. Energy and material science problems of launching into space and descent to Earth of the device with low overloads. Kosm. nauka tehnol. 2002 ;8(Supplement2):469-475.

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