HTPB/GOX Hybrid Rocket Motor Test (Dec. 16, 2005)

Rocket Propulsion

0910412 / 0910512

 

Hybrid Rocket Motor Design Project.  One of the main components of this course was the semester design project in which each student team designed, built and tested a 5 lbf thrust hybrid rocket motor.   The thrust chambers were fabricated from aluminum and the nozzles were fabricated from graphite.   Solid fuel grains consisting of HTPB and HTPB/Al were produced by each team.  The oxidizer was gaseous oxygen supplied at 500 SLPM.  The chamber pressure was constrained to 100 psig.  Each rocket was tested on a thrust stand that enabled the measurement of instanteous oxygen mass flow rate, chamber pressure and thrust.    With these data, each team was able to measure specific impulse (Isp), characteristic exhaust velocity (C*), thrust coefficient (Cf) and compare these measurements to their theoretical models, which predicted instaneous O/F, C*, Pc, and thrust. 

This website contains pictures, movies and test data from each of the rockets.  Enjoy!

 

Here is a power point presentation that describes the project and development of the thrust stand.

Instructor: Anthony J. Marchese                                     

home and objectives

Team 1.  Kyle Lick, Yahm Marx, Brian Scott and Harmon Kim. 

Fuel: 80% HTPB/ 20% Al      Oxidizer: GOX        Length of Fuel Grain: 12 in

Port Diameter: 0.5 in        Throat Diameter: 0.285   Ae/At: 3.65

Download Movie Here                                  Download Test Results Here

Team 2.  Dona Johnson, Larry Pologruto, Tim Vaughn, Marcos Villa-Gonzalez

Fuel: 80% HTPB/ 20% Al      Oxidizer: GOX        Length of Fuel Grain: 10.9 in

Port Diameter: 0.6 in        Throat Diameter: 0.25   Ae/At: 4.0

Download Movie Here                                  Download Test Results Here

Team 3.  Brian Thibaudeau, Will Weisnet and Mark Wessel

Fuel: HTPB       Oxidizer: GOX        Length of Fuel Grain: 12 in

Port Diameter: 0.75 in        Throat Diameter: 0.262  Ae/At: 4.17

Download Movie Here                                 Download Test Results Here

Team 4 (Stubby).  Joshua Forman, Kristen Grdinich, Jeff Giesecke and Dan Miller

Fuel: HTPB       Oxidizer: GOX        Length of Fuel Grain: 8.5 in

Port Diameter: 0.4 in        Throat Diameter: 0.24   Ae/At: 4.5

Download Movie Here                                 Download Test Results Here

Team 5 (Big Red).  Bob Erney, TJ Gray, Rob Kandetzke and Mike Melniczuk

Fuel:   HTPB       Oxidizer: GOX        Length of Fuel Grain: 12 in

Port Diameter: 0.5 in        Throat Diameter: 0.281   Ae/At: 4.0

Download Movie Here                                Download Test Results Here

For a complete archive of movies click here.

For a complet archive of photos click here.

Is the valve open?

course outline and notes

homework assignments

NASA CEA Code

rocket of the week

links and combustion research

rules and grading

Rowan University • 201 Mullica Hill Road • Glassboro, New Jersey 08028 • Phone / 856.256.5343
Contact  marchese@rowan.edu with questions, problems or comments.
©2005 Anthony J. Marchese.