发明名称 HYBRID PARACHUTE
摘要 <p>A hybrid parachute, method of deploying a parachute and method of landing a payload. The hybrid parachute utilizes a reefing system that provides for the initial deployment of a deceleration stage that is configured to withstand the stresses of high-speed and/or high altitude openings. The deceleration stage has operating characteristics similar to known high-speed parachutes. After sufficient deceleration has been achieved with the deceleration stage, reefings are released deploying one or more low-speed high drag stages of the device. The high drag stage(s) provide the landing characteristics of a low-speed parachute, including the possibility of controlled descent and landing.</p>
申请公布号 WO2009038586(A1) 申请公布日期 2009.03.26
申请号 WO2007US79210 申请日期 2007.09.21
申请人 JAMESON, NICHOLAS F.;PIONEER ASTRONAUTICS 发明人 JAMESON, NICHOLAS F.
分类号 B64D17/02 主分类号 B64D17/02
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