Investor Presentaiton
Advantages of AM
Improving functionality
Traditional Manufacturing
1. Time consuming and
cost intensive process
to produce
2.Increased risk of
human error due to
requirement of multiple
parts for single
component.
Monolithic Thrust
Chamber
Core element of a liquid-
propellant rocket engine.
Measurements:
228X194X310mm
3.Essential cooling
structure
manufactured
separately
Material: IN718 (Nickel
Superalloy)
Machine: SLMⓇ 280
Bedro
Co
Demo
Owigon plan
Source: SLM; NASA; G. P. Sutton, History of Liquid Propellant Rocket Engines, AIAA, Reston, VA, 2006.
Additive Manufacturing
1. Production time
decreased from ~6
months to <5 days
2.Entire component
printed, without needing
multiple parts -
significantly improving
reliability.
3.Innovative lattice
structure enabling an
integrated cooling
function which also
resulted in increased
stability.
SLM
SOLUTIONS
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