发明名称 |
PROPULSION SYSTEM OF SPACE OBJECT AND HYDRAULIC CONDENSER THEREFOR |
摘要 |
FIELD: space.SUBSTANCE: invention relates to aerospace engineering and can be used in propulsion units of space objects. Propulsion unit of space object comprises a cryogenic tank with a delivery valve and booster by a turbo pump, high-pressure cylinder with gaseous cryogenic component for booster turbopump turbine spin-up, cruise engine with turbo pump unit, hydraulic capacitor. Hydraulic condenser comprises casing with damper pipe with wall with holes directed along flow of liquid cryogenic component from cryogenic tank in cruise engine.EFFECT: invention improves energy and weight characteristics of propulsion units of space objects.2 cl, 2 dwg |
申请公布号 |
RU2583994(C2) |
申请公布日期 |
2016.05.10 |
申请号 |
RU20140137627 |
申请日期 |
2014.09.16 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "RAKETNO-KOSMICHESKAJA KORPORATSIJA "ENERGIJA" IMENI S.P. KOROLEVA" |
发明人 |
SMOLENTSEV ALEKSANDR ALEKSEEVICH;TUPITSYN NIKOLAJ NIKOLAEVICH;TUMANIN EVGENIJ NIKOLAEVICH;BELOV ALEKSEJ ALEKSANDROVICH;ROZHKOV MIKHAIL VIKTOROVICH |
分类号 |
B64G1/24;F02K9/00 |
主分类号 |
B64G1/24 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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