| Task |
Experimental Hypervelocity Missile
- Different payloads for sound tests of components and sub-systems
at hypervelocity flight conditions
- Possibility to investigate different motor types /dual pulse,
base bleed)
|
| Customer |
BWB / BMVg
|
| Technology |
High performance smoke reduced component propellant
- conical CFRP-Case
- missile velocity capability up to March 7
|
| Milestones |
- Contract 1999
- Design, Manufacturing, Static Tests 2000-2001
- Test flights
-
6th Feb 2002
-
23th Oct 2003
|
|
Hypervelocity motor on the test bench
|
