Header image  

Florida Institute of Technology

Rocket Team 2006

 
  [ HOME ]  
 
 
Mission

Summary

Mishaal Ashemimry

              The goal for this project is to send a spin stabilized rocket to the peak of the troposphere, or approximately 60,000 feet (18.28 km).  During ascent, the rocket will expel fuel exhaust with aluminum particles.  These aluminum particles are detectable by radar (borrowed from the Naval Base at Cape Canaveral) and can be interpreted into data by meteorologists in terms of winds or circulation in the atmosphere.  Any type of circulation in the air can be a sign of adverse weather, so any detection of strong winds or circulation could signal the possibility of a storm, which may or may not affect the launch schedule.

              Once the rocket has reached its maximum altitude, it will come down via parachute. The slow decent of the rocket by parachute will allow data to be collected in the atmosphere.  The meteorology team members propose to add equipment and sensors that are capable of measuring water vapor in the air, which in turn can be interpreted into the relative humidity.  The relative humidity can be used to predict adverse weather by means of cloud formation.  Such data collections would be an improvement to current meteorology methods and an asset to meteorology and NASA.

              Upon recovery of the rocket, depending on the amount of damage, it can be rebuilt and reused.  Even without knowing the total replacement cost of a weather balloon and radiosonde, our rocket will still be far less expensive to replace.  Truly, only time will tell if the rocket is not only more accurate, but less expensive than the weather balloons. 

Funding and Budget

              The following budget is based off of the final cost of the SOAR rocket.  The Surveyor is significantly smaller then SOAR, only 13 ft, and the payload is much less complicated.  This means that the overall stock materials cost will be lower and the budget for the payload can be reduced significantly.  A total of $8999 must be raised to pay for the rocket.  The process of securing funding must begin immediately.

 

              Preliminary Budget

3

 

S

Glen Guzik

09.13.05

Items

Estimated Cost

 

 

Design and Testing: Jacque Frederick and Mishaal Ashemimry

 

 

Booster

$1,000.00

Ignition System

$150.00

Travel

$100.00

Fins

$350.00

Main Structure

$450.00

Frame to mount payload,

$300.00

Nose Cone

$650.00

Window (for camera)

$300.00

Services and Misc.

$150.00

Sub Total: Propulsion

$3,450.00

 

 

 

 

Construction:  Kenneth Schmidt

 

 

Endmills, Drills, ect.

$600.00

Travel

$400.00

Sub Total: Sustainer

$1,000.00

 

 

 

 

Safety: Jacque Frederick

 

 

Parachute Recovery System

$200.00

Travel

$100.00

Sub-Total: Safety

$300.00

 

 

 

 

Telemetry and Sensors: open

 

 

Payload

$400.00

Travel

$100.00

camera, & insulated material

$1,000.00

Sub-Total: Telemetry and Sensors

$1,500.00

 

 

 

 

Material Location: Saata Senii

 

 

Travel

$150.00

Truck Rental

$300.00

Sub-Total: Material Location

$450.00

 

 

 

 

Launch Coordination: Ruth Galaviz

 

 

Team Member and Rocket Transportation

$1,500.00

to Launch Facility

 

Incidental Expenses

300

Sub-Total: Launch Coordination

$1,800.00

 

 

 

 

Funding Acquisition and Team Promotion: Glen Guzik

 

 

Publicity:

$199.00

     Advertisements, Showcases, etc…

Contingency:

$300.00

Team Shirts

Sub-Total: Miscellaneous Expenses

$499.00

 

 

 

 

 

 

Work Study Students

 

 

Labor

0

Travel

$100.00

 

 

Sub-Total Work Study Students

$100.00

Grand Total:

$8,999.00

Contact Information

Mishaal Ashemimry – Team Leader

mishaal@ashemimry.com

321-373-5919 (home)

305-613-1111 (cell)

Glen Guzik – Dev Contact

gguzik@fit.edu

225-955-3388 (cell)

 

Random Pictures: