发明名称 Three stage rocket vehicle with parallel staging
摘要 A three stage rocket vehicle (11) having a large forward propellant tank (12) and a small aft propellant tank (13) axially aligned. Secured to the rear end of the aft propellant tank (13) is an engine mount structure (14) carrying rocket engines (15). Offset and secured to the propellant tanks (12,13) is a payload structure (18). The propellants from the large forward tank (12) are fed into the aft propellant tank (13) and the rocket engines (15) are fed propellants from the aft propellant tank (13). This arrangement enables the vehicle to parallel stage its use of engines and components.
申请公布号 US4451017(A) 申请公布日期 1984.05.29
申请号 US19820431886 申请日期 1982.09.30
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR, NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 MARSHALL, WILLIAM R.
分类号 B64G1/00;B64G1/40;B64G1/64;(IPC1-7):B64G1/40 主分类号 B64G1/00
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