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Unified Tactical Missile Kinetic Performance Model
AVT-321 Technical Course
CONCEPT DEFINITION
NEW MISSILE SYSTEM
FIRST STEP
TOWARDS
MISSON REQUIREMENTS
SIZE PERFOR-
MANCE
TYPE/SIZE OF THE
PROPULSION SUB-SYSTEM
UNIFIED TACTICAL
MISSILE KINETIC
PERFORMANCE MODEL
Consistency
Interoperability
Collaboration enhancement
Tactical missiles can strike and intercept targets on land, in the air and at sea. NATO needs to maintain a capability edge over potential adversaries with new and upgraded missile systems.
Concept definition is the first step towards a new missile system. Mission requirements will determine the size and performance of a system. Both are strongly related to the type and size of the propulsion sub-system.
Currently, to perform conceptual design, military users, procurement agencies and defense contractors in NATO nations use individual proprietary models and different data bases. This leads to non-consistent results and is hindering collaboration.
Watch the video!
The students learn how to select a surface or air-launched mission trajectory and define the size and shape of a missile body.
They learn how to define the appropriate propulsion system choosing between • a Solid Propellant Rocket motor,
which is still the most common choice today.
• a Throttleable Ducted Rocket, an advanced air-breathing system for missions demanding long range and sustained high speed
• or potential future candidates for tactical missile propulsion like a rocket motor with gelled fuel, a hybrid rocket motor or a Solid Fuel Ramjet
TASK GROUP
A task group formed by the Applied Vehicle Technology Panel of NATO’s Science and Technology Organization has leveraged the expertise of defense contractors, research organizations and governmental agencies from five NATO nations to create a unified tactical missile kinetic performance model.
COURSE INFORMATION
• Duration: 3-Day-Course • Attendees: 20-30 students per course • Course fee: 160 Euro per participant*
• no specialized knowledge is required
*excluding accommodation, traveling etc.
The model provides consistency and interoperability in defense planning studies and can eliminate barriers for collaboration. It allows the user to create basic design of a tactical missile with a choice of different propulsion subsystems. In addition, the code offers an option to apply Thrust Vector Control and has an easy to use Graphical User Interface.
Locations and times: 04 - 06 June 2019
NATO School Oberammergau Oberammergau, DEU
27 – 29 August 2019 NATO Joint Warfare Center Stavanger, NOR
10 – 12 September 2019 German Aerospace Center (DLR) Washington D.C., USA
17 – 19 September 2019 Lancaster University Center Lancaster, CA, USA
Organization: Dr. Norman Hopfe, DEU Mr. Jason Mossman, USA
Presenter: Dr. Norman Hopfe, Bayern-Chemie, DEU Mr. Jason Mossman, AFRL, USA Dr. Erland Orbekk, NAMMO, NOR Mr. Ronald Veraar, TNO, NLD
NATO S&T TASK GROUP If you are interested in attending the course or would like to request any further information, please contact Dr. Norman Hopfe via eMail [email protected] or visit the NATO STO Webpage:
If you are unable to enroll via the internet, please contact NATO Collaboration Support Office (CSO) OCD Enrolment Coordinator Anne Reboul phone +33 (0)1 55 61 22 67 email [email protected]
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