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Suborbital Reentry Flight Demonstration for 2.5 m Deployable Inflatable Flexible Aeroshell Using Sounding Rocket

Year: 2025

Type: article

Source: Journal of Spacecraft and Rockets

DOI: 10.2514/1.a36152

Authors: Yasunori Nagata, Kazuhiko Yamada, Tatsuro Nakao, Hitoshi Hamori

Institution: Japan Aerospace Exploration Agency

Language: English

Topic: Aerospace Engineering and Energy Systems

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W7101399738

FWCI: 0.391

Cites: 19

Cited by: 1

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