SU1785188A1 - SYSTEM OF THERMAL REGULATION OF PILOTED SPACE APPARATUS - Google Patents

SYSTEM OF THERMAL REGULATION OF PILOTED SPACE APPARATUS

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Publication number
SU1785188A1
SU1785188A1 SU3015473/23A SU3015473A SU1785188A1 SU 1785188 A1 SU1785188 A1 SU 1785188A1 SU 3015473/23 A SU3015473/23 A SU 3015473/23A SU 3015473 A SU3015473 A SU 3015473A SU 1785188 A1 SU1785188 A1 SU 1785188A1
Authority
SU
USSR - Soviet Union
Prior art keywords
radiator
liquid
heat exchangers
piloted
section
Prior art date
Application number
SU3015473/23A
Other languages
Russian (ru)
Inventor
К.А. Коптелов
Р.М. Копяткевич
О.В. Сургучев
В.М. Цихоцкий
Original Assignee
Научно-производственное объединение "ЭНЕРГИЯ"
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Научно-производственное объединение "ЭНЕРГИЯ" filed Critical Научно-производственное объединение "ЭНЕРГИЯ"
Priority to SU3015473/23A priority Critical patent/SU1785188A1/en
Application granted granted Critical
Publication of SU1785188A1 publication Critical patent/SU1785188A1/en

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  • Control Of Temperature (AREA)

Abstract

1. Система терморегулирования пилотируемого космического аппарата, включающая внутренние контуры теплосъема и влагосъема, связанные через жидкостно-жидкостные теплообменники с секциями радиатора-излучателя и содержащие гидроблоки и регуляторы расхода, связанные через блок автоматики с датчиками температуры, отличающаяся тем, что, с целью повышения надежности и увеличения ресурса системы, в нее введена магистраль, содержащая гидроблок и соединяющая выходы жидкостно-жидкостных теплообменников с входами секций радиатора-излучателя, при этом секции радиатора-излучателя и жидкостно-жидкостных теплообменников связаны между собой последовательно, а регулятор расхода установлен на выходе одной из секций радиатора-излучателя и связан через блок автоматики с датчиком температуры, помещенным в отсеке.2. Система по п.1, отличающаяся тем, что регулятор расхода выполнен в виде регулируемого дроссельного устройства.1. Thermal control system of a manned spacecraft, including internal circuits of heat removal and moisture removal, connected via liquid-liquid heat exchangers to radiator-emitter sections and containing hydraulic units and flow regulators connected through an automation unit to temperature sensors and increasing the resource of the system, a line is inserted into it containing a hydraulic block and connecting the outlets of liquid-liquid heat exchangers with the inputs of radiator-emitter sections, p and this section of the radiator and the radiator-liquid-liquid heat exchangers connected in series, and a flow regulator mounted at the outlet of one section, heat sink and the radiator is connected via automation unit with a temperature sensor placed in otseke.2. A system according to claim 1, characterized in that the flow regulator is designed as an adjustable throttle device.

SU3015473/23A 1981-04-06 1981-04-06 SYSTEM OF THERMAL REGULATION OF PILOTED SPACE APPARATUS SU1785188A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3015473/23A SU1785188A1 (en) 1981-04-06 1981-04-06 SYSTEM OF THERMAL REGULATION OF PILOTED SPACE APPARATUS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3015473/23A SU1785188A1 (en) 1981-04-06 1981-04-06 SYSTEM OF THERMAL REGULATION OF PILOTED SPACE APPARATUS

Publications (1)

Publication Number Publication Date
SU1785188A1 true SU1785188A1 (en) 2005-12-20

Family

ID=60536607

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3015473/23A SU1785188A1 (en) 1981-04-06 1981-04-06 SYSTEM OF THERMAL REGULATION OF PILOTED SPACE APPARATUS

Country Status (1)

Country Link
SU (1) SU1785188A1 (en)

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