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Merlin rocket engine--How (and Why) SpaceX Will Colonize Mars - Page 4 of 5 - Wait But Why | Page 4

Merlin rocket engine--How (and Why) SpaceX Will Colonize Mars - Page 4 of 5 - Wait But Why | Page 4

NASA Standards Mechanical tests – Strength – Sinusoidal sweep vibration (5 to 50 hertz [Hz]) ELV and STS payloads – Random vibration and acoustics – Shock.

NASA Standards Mechanical tests – Strength – Sinusoidal sweep vibration (5 to 50 hertz [Hz]) ELV and STS payloads – Random vibration and acoustics – Shock.

D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB 2014-2015 PDR PRESENTATION 1.

D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB 2014-2015 PDR PRESENTATION 1.

D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB 2014-2015 PDR PRESENTATION 1.

D EPARTMENT OF M ECHANICAL AND A EROSPACE E NGINEERING HIGH POWERED ROCKETRY CLUB 2014-2015 PDR PRESENTATION 1.

Our Mission Statement  Launch a high-power rocket to an altitude of one mile carrying the Operation: Epic Beep payload package. At lift off, the rocket’s.

Our Mission Statement  Launch a high-power rocket to an altitude of one mile carrying the Operation: Epic Beep payload package. At lift off, the rocket’s.

 Vehicle dimensions, materials, and justifications  Static stability margin  Plan for vehicle safety verification and testing  Baseline motor selection.

 Vehicle dimensions, materials, and justifications  Static stability margin  Plan for vehicle safety verification and testing  Baseline motor selection.

Flight Readiness Review Team Hawaii. Vehicle Properties Diameter (in)6 inches Length (in)127 inches Gross Liftoff Weight (lb)50.25 lb Launch Lug/button. -  ppt download

Flight Readiness Review Team Hawaii. Vehicle Properties Diameter (in)6 inches Length (in)127 inches Gross Liftoff Weight (lb)50.25 lb Launch Lug/button. - ppt download

Illinois Space Society Tech Team USLI CDR Presentation.

Illinois Space Society Tech Team USLI CDR Presentation.

Flight Readiness Review Atomic Aggies. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: 117.14 inches Approximate Loaded Weight: 35.25 lb.

Flight Readiness Review Atomic Aggies. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: 117.14 inches Approximate Loaded Weight: 35.25 lb.

NASA Standards Mechanical tests – Strength – Sinusoidal sweep vibration (5 to 50 hertz [Hz]) ELV and STS payloads – Random vibration and acoustics – Shock.

NASA Standards Mechanical tests – Strength – Sinusoidal sweep vibration (5 to 50 hertz [Hz]) ELV and STS payloads – Random vibration and acoustics – Shock.