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|
|Propellant mass||~ 290 kg|
|Apogee||~ 180 km|
Maria Holmström, Project manager, (SSC)
Andreas Stamminger, Campaign Manager (DLR Moraba)