Precooled turbojet engine flight experiment using balloon-based operation vehicle

K. Fujita*, S. Sawai, H. Kobayashi, N. Tsuboi, H. Taguchi, T. Kojima, K. Okai, T. Sato, Koji Miyaji

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

15 Citations (Scopus)


Development of the Balloon-based Operation Vehicle (BOV) is currently in progress for the first flight scheduled in 2006. In a series of BOV experiments, a vehicle in a wing-body configuration is lifted by a high-altitude balloon and dropped, after which the microgravity experiments will be performed onboard the vehicle under favor of the quasi-free-fall environments. Although the BOV is originally designed for the microgravity experiments, various types of experiments can also be performed in a hypersonic flight at lower altitudes. One candidate currently under review is a flight experiment of a precooled turbojet engine in reduced dimension. In this article, an overview of the BOV experiment is introduced, and the current development status of the BOV and a flight model of the precooled turbojet engine is presented. The aerodynamic load and the aerodynamic characteristics of the BOV are obtained by computational fluid-dynamic analyses and wind-tunnel experiments.

Original languageEnglish
Pages (from-to)263-270
Number of pages8
JournalActa Astronautica
Issue number1-5
Publication statusPublished - 2006 Jul
Externally publishedYes

ASJC Scopus subject areas

  • Aerospace Engineering


Dive into the research topics of 'Precooled turbojet engine flight experiment using balloon-based operation vehicle'. Together they form a unique fingerprint.

Cite this