JAXA logo labeled.
May 19, 2011 (JST)
The Japan Aerospace Exploration Agency (JAXA) successfully conducted the first phase of the "Drop test for Simplified Evaluation of Non-symmetrically Distributed sonic boom*1" (D-SEND) twice on May 7 and 16, 2011 (Sweden Standard Time) at the Esrange Space Center in Sweden in cooperation with the Swedish
Space Corporation (SSC). JAXA has, for the first time in the world, confirmed the validity of low sonic boom axisymmetric*2 design by a balloon drop test.
Establishing low sonic boom design technology is one of the highest priority issues for realizing silent supersonic transport. As part of silent supersonic research, JAXA is carrying out the two phased D-SEND project to validate its low sonic boom design concept and to contribute to the deliberation of
international standards for sonic booms based on the acquired data.
In the first phase called D-SEND#1, two different axisymmetric bodies were dropped from a balloon, and the sonic booms, measured both in the air and on the ground, were compared with each other. Through this test, JAXA has successfully demonstrated its low sonic boom axisymmetric design concept technology which reduced the sonic boom by half.
The data obtained from the test is valuable as a reference for the validation of the sonic boom propagation analysis method and is expected to contribute to low-sonic boom studies in the future. JAXA has also established for the first time a new method of demonstrating the low sonic boom design concept in the
form of a balloon drop test.
JAXA expresses our sincere gratitude to the Swedish Space Corporation and all parties that provided assistance in this demonstration test.
Space Corporation (SSC). JAXA has, for the first time in the world, confirmed the validity of low sonic boom axisymmetric*2 design by a balloon drop test.
Establishing low sonic boom design technology is one of the highest priority issues for realizing silent supersonic transport. As part of silent supersonic research, JAXA is carrying out the two phased D-SEND project to validate its low sonic boom design concept and to contribute to the deliberation of
international standards for sonic booms based on the acquired data.
In the first phase called D-SEND#1, two different axisymmetric bodies were dropped from a balloon, and the sonic booms, measured both in the air and on the ground, were compared with each other. Through this test, JAXA has successfully demonstrated its low sonic boom axisymmetric design concept technology which reduced the sonic boom by half.
The data obtained from the test is valuable as a reference for the validation of the sonic boom propagation analysis method and is expected to contribute to low-sonic boom studies in the future. JAXA has also established for the first time a new method of demonstrating the low sonic boom design concept in the
form of a balloon drop test.
JAXA expresses our sincere gratitude to the Swedish Space Corporation and all parties that provided assistance in this demonstration test.
*1 sonic boom
A sonic boom is a kind of impulsive sound of shockwaves, similar to thunder,
generated by supersonic flight
*2 axisymmetric
Typical axisymmetric shapes include cone, cylinder, etc.
For more details, please refer to the following website: http://www.apg.jaxa.jp/eng/index.html
1. Test details
Two test bodies, namely the N-wave model and the low-boom model are dropped consecutively from an altitude of 20-30km. The sonic boom generated by the free-fall is measured by using a low-boom measurement system and a boom measurement system.
Sequence of D-SEND#1
Place: Swedish Space Corporation (SSC), at Esrange Test Site (Kiruna, Sweden)
Role Sharing: Measurement of sonic booms in the air and on the ground (JAXA)
Management of measurement balloon and dropping of test models (SSC)
2. Test conditions
Correlation of velocity and altitude after the release
Preparation of balloon and test models(1st test) /
Balloon ascending into the sky (1st test)
3. Measurement Results
Pressure metamorphose time records measured by microphones in the air altitude of 500m (Pressure signature) are described below.
The characteristic N-type wave was clearly measured by N Wave Model (NWM) in the tests. Meanwhile, the low-boom model validated that its sonic boom could be reduced by comparing NWM.
4. Schedule of future tests
We will further analyze the obtained data and then report the results at a meeting of the SuperSonic Task Group (SSTG) of the International Civil Aviation Organization (ICAO) *3 in November.
*3 ICAO
ICAO is one of the specialized agencies of the United Nations Economic and Social Council, and codifies the treaty, international standard, recommendation and guideline related to international air services to ensure economical and substantial operation of the international air transportation business based on the principle of equal opportunity.
Mission website:
Research on Super/Hyper Sonic Airplane: http://www.jaxa.jp/projects/aero/sst/index_e.html
http://www.jaxa.jp/press/2011/05/20110519_dsend_e.html#ref
Images, Graphics, Text, Credit: Japan Aerospace Exploration Agency (JAXA).
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