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HYFLEX (Hypersonic Flight Experiment) was a National Space Development Agency of Japan reentry demonstrator prototype which was launched in 1996 on the only flight of the J-I launcher. It was a successor of OREX and was a precursor for the Japanese space shuttle HOPE-X.
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space hypersonic j-i 110 68 mi flight 1996 succeeded pacific experiment reentry launched tiles used hope well body data lifting
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| HYFLEX | Apogee | 110 km (68 mi) | 1.00 | infobox |
| HYFLEX | Dimensions | Length:4.40 m (14.4 ft) Span:1.36 m (4 ft 6 in) Height:1.04 m (3 ft 5 in) | 1.00 | infobox |
| HYFLEX | Disposal | splashed down recovery failed | 1.00 | infobox |
| HYFLEX | Landing date | February 11, 1996 (1996-02-11) | 1.00 | infobox |
| HYFLEX | Landing site | Pacific Ocean near Chichi-jima | 1.00 | infobox |
| HYFLEX | Launch date | February 11, 1996 (1996-02-11) | 1.00 | infobox |
| HYFLEX | Launch mass | 1,054 kg (2,324 lb) | 1.00 | infobox |
| HYFLEX | Launch site | LA-N, Tanegashima Space Center | 1.00 | infobox |
| HYFLEX | Manufacturer | Mitsubishi Heavy Industries | 1.00 | infobox |
| HYFLEX | Operator | NASDA | 1.00 | infobox |
| HYFLEX | Rocket | J-I | 1.00 | infobox |
| HYFLEX | Website | At JAXA.jp | 1.00 | infobox |
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