发明名称 Gas storage and feed system for rocket propelled launch vehicle has insulated cylinder heated by internal heat exchanger
摘要 The pressurised gas storage and feed system consists of a cylinder (12) with sufficient structural integrity for the stored fluid, inlet and outlet flow regulators, and an internal heater to control the gas pressure. The heater is in the form of a heat exchanger (18) carrying a heated transmission medium such as a stored gas heated in a separate heat exchanger by hot gases from a rocket motor. The cylinder, which has a pressure casing of forged and welded titanium, is designed to store helium in a supercritical state at about 4600 psi and 20 Deg R.
申请公布号 FR2825135(A1) 申请公布日期 2002.11.29
申请号 FR20020006167 申请日期 2002.05.21
申请人 LOCKHEED MARTIN CORPORATION 发明人 BECK PHILIP;KUTTER BERNARD;ZEGLER FRANK
分类号 B64G1/40;F02K9/50;F17C1/00;F17C7/02;F17C7/04;F17C13/00;F17C13/08;(IPC1-7):F17C7/02;F17C1/12;F17C5/04 主分类号 B64G1/40
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