Olovarenko UV. Increasing of reliability of large demension bellow in launch vehicle fuel system. Kosm. nauka tehnol. 2001 ;7(Supplement1):040-043.

Nakashidze LV, Zarivnyak GL, Mitrokhov SA. On use of optimum operation mode of solar cell. Kosm. nauka tehnol. 2001 ;7(Supplement1):038-039.

A. Zhivotov Y. Liquid balancing device for static balancing under constant final liquid flow rate. balancing accuracy. Kosm. nauka tehnol. 2001 ;7(Supplement1):033-037.

Artyukhova TP. On elastic stability of three layer payload fairing with discrete longitudinal links for launch vehicle. Kosm. nauka tehnol. 2001 ;7(Supplement1):030-033.

Artyukhova TP. Definition of critical loading of loss of stability for three layer payload fairing with elastic longitudinal joints. Kosm. nauka tehnol. 2001 ;7(Supplement1):025-029.

Andryukov RA, Zemlyanoy KN, Dubets SV. Guaranteed power system supply of systems and equipment participating in preparation and start of a rocket booster. Kosm. nauka tehnol. 2001 ;7(Supplement1):023-024.

Arlekinova ОЕ. Study of load parameters of ILV «ZENIT-3SL» during its standing at the launch platform. Kosm. nauka tehnol. 2001 ;7(Supplement1):020-022.

Arlekinova ОЕ, Vasilenko AA. Estimate of predictable loading on the base cross-section of ILV «ZENIT-3SL». Kosm. nauka tehnol. 2001 ;7(Supplement1):018-020.

¹Fedorov OP. Introductory word. Kosm. nauka tehnol. 2001 ;7(Supplement1):005.

Baibuz OG, Zemlyanaya SV, Pristavka FA. Strategy comparison for space vehicles' active existence terms estimation during protracted acceptance testing. Kosm. nauka tehnol. 2001 ;7(Supplement1):015-018.