LEON II PDR
LOX/LCH4 Rocket Engine
Left to right: Tyler Woods, Ted W. Bohrer, Kyle DuPriest, Justin Ancheta,
Emelon Bit Atanus,Teddy Hendriks, Sebastian Klukas.
Goal & Success Criteria
A LOX/LCH4 Rocket Engine
Design, build, and test GOX/CH4 engine to test control system
Design, build, and test H2O2/Kerosene engine
Benchmark against Aerobee engines
Achieve 250 lbs of thrust at 350 psi
What is LEON III?
Senior Project Lead: Francis Bostick
Propulsion for CubeSats
Design a thruster viable for a 1U-2U CubeSat
Lab: MIPSI for a dynamic system
(one lab per group)
PreLab: Brainstorm a physical system with an interesting question (not a Ph.D. dissertation), e.g., system
identification, design, stability, control, . . .
1. Picture of you and your team
Lecture 9: Equivalent Force-Couples (3D)
A truss is a rigid frame work usually
consists of beams, struts and bars to
resist deformation due to loads
In aircraft this type of frame work is
mainly used for fuselage and wings.
The truss constr
AE160 Aerodynamics I
Prof. Rachael Ishaya
Fluid Properties Workout Problem 1
Consider the pipe and the cylinder of the example problem done in class. However, in this case,
the cylinder in now slowing down as it falls. At a p