Abstract
Within the Japanese space plane program HOPE different generic vehicles such as OREX, AFLEX and HYFLEX were flown for both qualification and development purposes as well as validation. To improve the comprehension, four tests with a HYFLEX nose structure of original size were performed in the plasma wind tunnel facility SCIROCCO at CIRA, Italy. Within the cooperation between the Japanese space agency JAXA, CIRA and IRS a catalysis based sensor system for the measurement of the local dissociation degree was developed, integrated and applied. The facilities for the qualification at IRS, SCIROCCO and the sensor design are described. A methodology to derive the dissociation degree and corresponding results are shown.
| Original language | English |
|---|---|
| Title of host publication | Collection of Technical Papers - 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference |
| Pages | 575-583 |
| Number of pages | 9 |
| Volume | 1 |
| Publication status | Published - 2006 |
| Externally published | Yes |
| Event | 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference - San Francisco, CA Duration: 2006 Jun 5 → 2006 Jun 8 |
Other
| Other | 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference |
|---|---|
| City | San Francisco, CA |
| Period | 06/6/5 → 06/6/8 |
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ASJC Scopus subject areas
- Engineering(all)
Cite this
Determination of local dissociation degree for HYFLEX nose structure tests in SCIROCCO. / Auweter-Kurtz, M.; Caristia, S.; Fertig, M.; De Fillipis, F.; Herdrich, G.; Löhle, S.; Morino, Y.; Pidan, S.; Schussler, M.
Collection of Technical Papers - 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Vol. 1 2006. p. 575-583.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Determination of local dissociation degree for HYFLEX nose structure tests in SCIROCCO
AU - Auweter-Kurtz, M.
AU - Caristia, S.
AU - Fertig, M.
AU - De Fillipis, F.
AU - Herdrich, G.
AU - Löhle, S.
AU - Morino, Y.
AU - Pidan, S.
AU - Schussler, M.
PY - 2006
Y1 - 2006
N2 - Within the Japanese space plane program HOPE different generic vehicles such as OREX, AFLEX and HYFLEX were flown for both qualification and development purposes as well as validation. To improve the comprehension, four tests with a HYFLEX nose structure of original size were performed in the plasma wind tunnel facility SCIROCCO at CIRA, Italy. Within the cooperation between the Japanese space agency JAXA, CIRA and IRS a catalysis based sensor system for the measurement of the local dissociation degree was developed, integrated and applied. The facilities for the qualification at IRS, SCIROCCO and the sensor design are described. A methodology to derive the dissociation degree and corresponding results are shown.
AB - Within the Japanese space plane program HOPE different generic vehicles such as OREX, AFLEX and HYFLEX were flown for both qualification and development purposes as well as validation. To improve the comprehension, four tests with a HYFLEX nose structure of original size were performed in the plasma wind tunnel facility SCIROCCO at CIRA, Italy. Within the cooperation between the Japanese space agency JAXA, CIRA and IRS a catalysis based sensor system for the measurement of the local dissociation degree was developed, integrated and applied. The facilities for the qualification at IRS, SCIROCCO and the sensor design are described. A methodology to derive the dissociation degree and corresponding results are shown.
UR - http://www.scopus.com/inward/record.url?scp=33751419775&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=33751419775&partnerID=8YFLogxK
M3 - Conference contribution
SN - 1563478110
SN - 9781563478116
VL - 1
SP - 575
EP - 583
BT - Collection of Technical Papers - 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
ER -