Attitude dynamics for flare-type membrane aeroshell capsule in reentry flight experiment

Yasunori Nagata, Kazuhiko Yamada, Takashi Abe, Kojiro Suzuki

Research output: Chapter in Book/Report/Conference proceedingConference contribution

11 Citations (Scopus)

Abstract

An inflatable decelerator is promising as atmospheric entry systems in the next generation. Although the various kinds of inflatable decelerators were proposed and researched in the past, we focus especially on a flare-type membrane aeroshell sustained by an inflatable torus. The flare-type membrane aeroshell may easily make re-entry systems simple and light-weighted because the aeroshell can be composed mainly of light-weighted membrane. As an important milestone of the development of the vehicle, a re-entry flight demonstration of the vehicle with the flare-type membrane aeroshell was carried out using Japanese S-310 sounding rocket in August, 2012. This flight experiment was successfully accomplished and various data, including the attitude of the vehicle during the supersonic atmospheric re-entry, was acquired. The attitude dynamics was qualitatively reconstructed base on the flight data, which shows that the vehicle entered into the atmosphere with high angle of attack and experienced a drastic attitude motion caused by the aerodynamic force. After the initial significant motion phase, the attitude behavior of the vehicle calmed down before the successive deceleration phase. That is, the vehicle made a flight with a normal attitude and, as planned, its attitude was almost stable after the atmospheric-entry. In all, it was confirmed that the attitude stability of vehicles with a flare-type membrane aeroshell could be realized on a supersonic atmospheric-entry.

Original languageEnglish
Title of host publicationAIAA Aerodynamic Decelerator Systems (ADS) Conference 2013
DOIs
Publication statusPublished - 2013
Externally publishedYes
Event22nd AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013 - Daytona Beach, FL, United States
Duration: Mar 25 2013Mar 28 2013

Other

Other22nd AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013
CountryUnited States
CityDaytona Beach, FL
Period3/25/133/28/13

Fingerprint

Reentry
Membranes
Experiments
Sounding rockets
Deceleration
Angle of attack
Aerodynamics
Demonstrations

ASJC Scopus subject areas

  • Aerospace Engineering
  • Electrical and Electronic Engineering

Cite this

Nagata, Y., Yamada, K., Abe, T., & Suzuki, K. (2013). Attitude dynamics for flare-type membrane aeroshell capsule in reentry flight experiment. In AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013 https://doi.org/10.2514/6.2013-1285

Attitude dynamics for flare-type membrane aeroshell capsule in reentry flight experiment. / Nagata, Yasunori; Yamada, Kazuhiko; Abe, Takashi; Suzuki, Kojiro.

AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013. 2013.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Nagata, Y, Yamada, K, Abe, T & Suzuki, K 2013, Attitude dynamics for flare-type membrane aeroshell capsule in reentry flight experiment. in AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013. 22nd AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013, Daytona Beach, FL, United States, 3/25/13. https://doi.org/10.2514/6.2013-1285
Nagata Y, Yamada K, Abe T, Suzuki K. Attitude dynamics for flare-type membrane aeroshell capsule in reentry flight experiment. In AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013. 2013 https://doi.org/10.2514/6.2013-1285
Nagata, Yasunori ; Yamada, Kazuhiko ; Abe, Takashi ; Suzuki, Kojiro. / Attitude dynamics for flare-type membrane aeroshell capsule in reentry flight experiment. AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013. 2013.
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