薄膜型高高度気球の新しい放球法の開発
松坂幸彦， 井筒直樹， 山上隆正 - JOURNAL OF THE JAPAN SOCIETY …, 2001 - jlc.jst.go.jp
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Study on Low-ballistic-coefficient Atmospheric-entry Technology using Flexible Aeroshell
K Yamada, Y Kimura, D Akita, T Abe… - … OF THE JAPAN …, 2009 - jstage.jst.go.jp
A Low-ballistic-coefficient atmospheric-entry technology using a flexible aeroshell is
promising for a space transportation system because it can reduce the aerodynamic heating …
promising for a space transportation system because it can reduce the aerodynamic heating …
Application of bioinstrumentation in developing a pressure suit for suborbital flight
P Llanos, E Seedhouse - 2016 - commons.erau.edu
Abstract/Description This presentation features Embry-Riddle Aeronautical University's U-2
pressure suit. Built to be light and cost-effective, this suit is comfortable, comes in multiple …
pressure suit. Built to be light and cost-effective, this suit is comfortable, comes in multiple …
Flying without Dying: The Future of Wingsuit Design
ME Ferguson - 2016 - openscholarship.wustl.edu
Wingsuit flying is an extreme sport practiced by veteran skydivers and BASE jumpers. From
1930 to the 1960s, the attempt to create a functional wingsuit killed 96% of pioneers …
1930 to the 1960s, the attempt to create a functional wingsuit killed 96% of pioneers …
Space Suits Technology
S Kibe, K Suzuki - Shinku, 1995 - jstage.jst.go.jp
宇 宙 服 の 技 術 Page 1 解 説 宇 宙 服 の 技 術 木 部 勢 至 朗*・ 鈴木 克 徳* (受理1995年3月
20日,掲 載決定1995年5月6日) Space Suits Technology Seishiro KIBE and Katsunori SUZUKI …
20日,掲 載決定1995年5月6日) Space Suits Technology Seishiro KIBE and Katsunori SUZUKI …
[PDF][PDF] 인력비행기스카이러너설계· 제작· 비행
이기영， 최성옥， 오장근 - 한국군사과학기술학회지, 2010 - Citeseer
With the financial sponsorship of FKI and six other companies, the design and construction
of the human powered aircraft Sky Runner has been begun to design in December of 2008 …
of the human powered aircraft Sky Runner has been begun to design in December of 2008 …
Suborbital reentry demonstration of inflatable flare-type thin-membrane aeroshell using a sounding rocket
K Yamada, Y Nagata, T Abe, K Suzuki… - Journal of Spacecraft …, 2015 - arc.aiaa.org
An inflatable decelerator is promising as a next-generation atmospheric-entry system owing
to its reduced aerodynamic heating and high packing efficiency. In this study, a suborbital …
to its reduced aerodynamic heating and high packing efficiency. In this study, a suborbital …
[PDF][PDF] Physiological Effects of a Mechanical Counter Pressure Suit
D Tourbier, A Hargens, P Webb… - … Meeting, Poster Session …, 2001 - researchgate.net
During extravehicular activity (EVA) life is normally supported by breathing oxygen at 222
mm Hg (4.3 psi) in a conventional full pressure suit, which pressurizes the entire body with …
mm Hg (4.3 psi) in a conventional full pressure suit, which pressurizes the entire body with …
Study on Mini Re-Entry System Using Deployable Membrane Aeroshell
M Koyama, K Suzuki, O Imamura… - TRANSACTIONS OF THE …, 2009 - jstage.jst.go.jp
An aeroshell made from membrane material have an advantage of reduction in the
aerodynamic heating, because its small mass and large area enable us to make the low …
aerodynamic heating, because its small mass and large area enable us to make the low …