The research will be carried out using an unguided solid propellant twostaged rocket, Terrier Mk12 and Improved Orion.
The Terrier motor has a burn phase of 5 seconds. The Imp. Orion Motor is a dual thrust burner with a boost phase of 5 seconds and a sustainer phase of approximately 21 seconds. The rocket accelerates the payload then for 40.0 seconds with peak acceleration during the boost phase of approximately 21 g.
| SSC Campaign Manager: | Maria Holmström |
| MORABA Campaign Manager: | Andreas Stamminger |
| MORABA Payload Engineer: | Markus Pinzer |
| Project Scientists: | Ali Gülhan |
| Fluid Mechanics | Andreas Henze |
| Launch site | Esrange Space Center |
| Launch date | July 19 at 06:05 LT |
| Rocket type | Terrier Mk12 / Improved Orion |
| Nominal payload diameter | 14 inches |
| Propellant type | composite |
| Propellant mass | ~ 290 kg |
| Apogee | ~ 180 km |
Maria Holmström, Project manager, (SSC)
maria.holmstrom@sscspace.com
Andreas Stamminger, Campaign Manager (DLR Moraba)
mailto:Andreas.Stamminger@dlr.de
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