A choice of spacecraft design parameters subject to operation efficiency requirements

2008, vol. 15, no. 1, pp. 37-43

Spacecraft and Rockets

Аuthors

Zolotov A. A.^*, Nepochatykh D. A.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: alexandrzolotov41@mail.ru

Abstract

A technique is suggested to choose spacecraft design parameters subject to operation efficiency requirements. Recommendations are formulated to evaluate effectiveness and to normalize reliability for spacecraft onboard equipment.

mai.ru — informational site of MAI