Integrated Life Support Power Supply Propulsion System on Electrochemical Principles for Space Station Moscow Aviation Institute

Format:

Conference/Event

Author/Creator:

Demidova, Nadejshda S., author.

Conference Name:

International Conference on Environmental Systems (1995-07-10 : San Diego, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1995

Summary:

Application of the reversible systemsas power accumulators working media generator opens the words for creation of the economic integrated life support-energy-propulsion complexes for the manned stations.The system includes on electrolyser which decomposes water into oxygen and hydrogen under influence of the solar panel electric power. From an accumulator these gases are used to ensure the periodical operation of the correction thrusters, orientation systems, in the maximum power demand modes and for cosmonauts breathing.This work describes:There is a plan for experimental development of the integrated electrical engine system on the small satellite for the orbital station servicing. For the 60W power consumption duty mode and the 210W maximum power demand mode the system ensures generation of the gas which is sufficient for the orbit keeping and has twice less mass with respect to the traditional scheme of "solar-buffer-chemical battery" and the autonomous engine

Notes:

Vendor supplied data

Publisher Number:

951560

Access Restriction:

Restricted for use by site license