University of Utah Unity IV Responsibilities Motor System –Fuel –Nozzle –Ignition Flight Profile Maximum Energy Footprint.

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Presentation transcript:

University of Utah Unity IV Responsibilities Motor System –Fuel –Nozzle –Ignition Flight Profile Maximum Energy Footprint

Motor System Fuel –HTPB: Fuel grain composed of R-45M resin –Cross- linked with diisocyanate Motor Housing –6061-T6 Aluminum –Static tested to 1200 psia Nozzle –Ceramic Composite –Rated to 5000 F

Ignition Model Rocket Motors –2, Estes C8-0 motors Accessible on Launch Rail Low power requirement –4 AA Batteries Reliable Performance

HTPB NO 2 inlet Estes C8-0 Motor Injector “O” Ring Seal Motor Cap Assembly

Flight Profile Maximum Altitude –10,641 feet AGL, at T = 28 seconds Burn Time –T = 5.4 seconds Flight Velocity –Launch Rail Exit = 89.1 ft/s –Overall Flight = 0.71 Mach FTS Failure Impact –763 ft/s at T=58 seconds

Maximum Energy Footprint 5.40 Miles at   =45 0 No Critical Areas with in Range

Motor Assembly

Motor Cap

Motor Housing

Motor Nozzle

Motor Nozzle Retainer

Motor Assembly

Fuel Mixing Procedure Safety Equipment Liquid Chemicals Incorporate By Hand Dry Chemicals Incorporate By Hand Mix For 30 Minutes

Fuel Mixing Problems Need More Mixing Time Recipe Catalyst

3” Motor Fuel Mixing

8” Motor Fuel Mixing

Modified Fuel Mixing Tank

Portable Oven Design 1

Portable Oven Design 2

Portable Oven Design 3

Mandrel Configurations