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公开(公告)号：WO2019021220A1
公开(公告)日：2019-01-31
申请号：PCT/IB2018/055563
申请日：2018-07-25
摘要： The present invention relates to a re-entry module comprising an alpha-dome comprising a petal structures [1-5, 49] positioned on the upper surface [7] of the base for enclosing the payload; Omega hexon positioned parallel to surface [9] and comprising of a base [16], a spike [24] and nozzle [15]; and a plurality of hexon positioned on the periphery of spike [24] wherein hexon is a modified scramjet engine having an outlet velocity vector positioned at an angle θ to the inlet velocity vector, wherein, omega hexon is provided with the inlet vents [26] positioned with spike [24] for the inflow of free stream air, a Delta area where fuel and compressed air interact and flame holders, and wherein, the gases formed will expand and pass through the aerospike nozzle [15], resulting in providing retro thrust to the re-entry module.
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