Project Coldfire

Home | What's New | Photos | Videos | Projects | Flight Data | Misc Info  | Links | Email

Home

What's New 

Photo Gallery

 

My Best Photos

Coldfire

Angelfire

Starfire

Wildfire

Vulcan

Scorpion

Nike Dart

Tempest

Black Widow

Sentinel

Hybrid Dart

Arcas

Scott's Rockets

The Early Years

Aerial Photos

Tripoli Idaho Photos

LDRS 26  (2007)

     Angelfire at LDRS 26

     Starfire    at LDRS 26

     Wildfire   at LDRS 26

     Scott's Flights at LDRS 26

LDRS 24  (2005)

Desert Heat 2006

Desert Heat 2005

Summer Skies 2007

Summer Skies 2006

Summer Skies 2005

Orange Crush Loop

XPRS 2007 Photos

XPRS 2006 Photos

     Starfire    at XPRS 2006

     Angelfire at XPRS 2006

     Wildfire   at XPRS 2006

     Nike Dart at XPRS 2006

XPRS 2005 Photos

XPRS 2004 Photos

FITS 2007 Photos

FITS 2006 Photos

FITS 2003 Photos

Vulcan Ignition

Other Photos

Video Gallery

 

Angelfire

Starfire

Wildfire

Vulcan

Scorpion

Other Videos

Video Help          

Projects

 

Coldfire

     Components

     Airframe fiberglassing

     Fin slots

     Motor tube construction

     Fin attachment

     Nitrous vent

     Booster bulkhead

     Fin fillets and finishing

     Nosecone

     Altimeter bay

     Recovery system

     Motor adapter & tailcone

     Decals

     Rail guides

Angelfire

     Booster

     Fin fillets

     Nosecone

     Altimeter bay

     Altimeter electronics

     GPS electronics

     Recovery components

     Painting

     Finishing

Starfire

      Booster

      Fins & motor tubes

      Fin slots

      Body tubes

      Coupler tubes

      Bulkheads

      Mirror hood

      Altimeter bay

      Antizipper band

      Antizipper straps

      Booster Elec-bay

      Camera module

      Camcorder module

      Paint & decals

      Rail guides

Wildfire

Vulcan

Scorpion

Nike Dart

GPS Radio Downlink

TV Transmitters

      Transmitter #1

      Transmitter #2

Launch Controller

G-switch Timer

Flight Data

 

Angelfire GPS Trajectories

Angelfire Altimeter Data

Flight Log

Misc Info

 

Altimeters

Altimeter Port Sizing

Altitude Charts

CAD Drawing Software

Centering Rings

Metal Plates

Delay Time Charts

Ejection Charge Sizing

Epoxy

Igniters

Launch Pads

Parachutes (etc)

Rocket Finding

Links

 

General Information

Clubs & Organizations

Rocketry Vendors

Kits and Components

Rocket Motors

Fun & Useful Sites

Electronics

Construction Supplies

Software Tools

Rocketry Magazines

Photographers

NASA

Email Vern

 

Coldfire is a scratch built custom design.  It is four inches in diameter and seven feet long. Construction started in January of 2006 and was on-and-off for a long time due to other time constraints.  However, it was finally completed in June 2007. 

The Coldfire airframe is flexible phenolic with two layers of fiberglass applied. The nosecone is plastic and the fins are G10 fiberglass.

Coldfire was specifically designed to fly on the HyperTEK hybrid motor system.  This system uses ABS plastic for fuel and liquid nitrous oxide (N2O) as the oxidizer.

The HyperTEK K240 motor uses an 835cc flight tank as shown at the right.  This motor burns for 5.6 seconds. It has a peak thrust of 96 lbs and an average thrust of about 52 lbs.

CAD drawing software information.

Coldfire is designed to deploy the main parachute at apogee. A dual deployment system was deemed unnecessary based on the expected altitudes and was also eliminated to save weight.  Coldfire should reach 4000 feet with the K240 hybrid motor. It can also fly on many different solid propellant motors to higher altitudes.

Coldfire has a large payload bay inside the nosecone that will be used to carry a GPS downlink transmitter system.

 

View Coldfire design drawings

This is 20 pages of detailed construction drawings!

Coldfire Specifications

Length: 7 feet, 1.5 inches  
Diameter: 4.02 inches
Weight: 12.5  lbs without motors  (Estimated)
Motor: 81mm motor tube fits Hypertek K240 835cc tank
Altimeters: Two MissileWorks RRC altimeters
Locator: Walston radio transmitter
Payload: GPS telemetry downlink
Parachute: Giant Leap TAC-1 72"
Built:  Started: Jan 2006.     Completed:  June 2007
First Flight: October 7, 2007 at Tripoli Idaho Birds-of-Prey launch
Construction: Body tube: Flexible Phenolic with two layers of 6 oz fiberglass

Fins:  G10 fiberglass

Nose cone:  5:1 Ogive, 3.9" diameter plastic "Pinnacle" nosecone from Giant Leap

Hypertek Hybrid Motor System

The photo above shows the 835cc flight tank mated with a HyperTEK "J" series grain to complete the K240 motor system.

The drawing at the left shows how the K240 hybrid motor is installed inside the Coldfire booster section.   Click on the image for a closer look.  The K240 motor is accessed by unscrewing the tail cone and then removing eight screws that hold the motor thrust plate onto the aft end of the booster. 

The overflow vent tube is a nylon set screw that has been drilled out lengthwise.  The screw threads hold it securely in place while allowing it to be easily installed and removed.

The HyperTEK product manual is a very good overview of the entire system. It describes the motors and the ground support equipment.

View HyperTEK product manual

Stability Analysis

 

Simulation Results

Motor: K240 HyperTek Hybrid
Maximum altitude:  4,362 feet
Maximum velocity:  316 MPH
Maximum acceleration:  4.81 g
Time to burnout:  6.76 sec.
Time to apogee:  18.34 sec.
Launch guide length: 96 in.
Velocity at launch guide departure: 33.1 MPH
The launch guide was cleared at: 0.53 sec
Liftoff  weight:  15.53 lbs
Simulation results for various motors.
 

Construction Photos

This photo shows all of the airframe parts for Coldfire ready to start assembly!  Click on it to see a page with details about individual parts. 

View information about each part

Airframe construction starts with four inch diameter phenolic tubing that is 48 inches long.  Two layers of 6 oz fiberglass were added along with an anti-zipper reinforcing steel band.  Click on the photo at the left to find out how this was done.

View airframe fiberglassing

The body tube for the booster section needed to have three lengthwise fin slots cut in it. Click on the photo at the left to see how that was done.

View process for cutting fin flots

Coldfire required a custom sized motor tube to hold the 81mm diameter Nitrous tank.   This photo shows the carbon fiber tube that was created.  Click on the photo or the link below to see how that was done.

View motor tube construction

Click on the photo at the left to see the whole process of aligning and attaching the fins to the motor tube.  It includes adding reinforcing strips of Kevlar at the fin root.

View fin attachment process

The HyperTEK nitrous flight system requires a special vent port in the side of the rocket.  Liquid nitrous will vent from this port to indicate the on-board flight tank is full.  Click on the photo or the link below to see how that was designed and built.

View construction of nitrous vent

The bulkhead at the top of the booster serves is a recovery system attachment point. A special reinforcement method was used to connect it to the top of the motor tube. See how that was done by clicking on the photo at the left or on the link below.

View booster bulkhead construction

 

The fin fillets were formed by using a small section of PVC pipe and some West System epoxy.   Click on the photo or the link below to see how that was done.  After that the booster section was sprayed with a filling primer and wet sanded to achieve a "perfect" surface finish.

View fin fillets and finishing

The Coldfire nosecone started out as a 5:1 Ogive "Pinnacle" nosecone from Giant Leap Rocketry.  However, a payload compartment was added inside the nosecone and a anchor point was added at the aft end that allows the nosecone to screw onto the body tube to secure it in place.  Click on the photo or the link below to see how all that works.

View nosecone construction

The Coldfire altimeter bay construction is a little bit different than is commonly used.  A special foam seal was created that isolates the ejection charge gasses from the electronics. Click on the photo or the link below to see how it was done.

View altimeter bay construction

The parachute flame protector is cut from a large piece of Kevlar cloth.  The recovery harness is made from tubular Kevlar and tubular nylon. Learn all about it by clicking on the photo or the link below.

View recovery harness construction

A special motor adapter tube and tail cone are used to secure the HyperTEK motor system inside Coldfire.  Click on the photo or the link below to see how that was designed and built.

View motor adapter and tail cone construction

Coldfire decals add a nice finishing touch.  Click on the photo or the link below to find out how they were made and applied.

 

View application of decals

Coldfire uses two linear rail guides available from Public Missiles.  A custom metal backer plate was used to hold them in place.  Click on the photo or the link below to see how that works.

View rail guide mounting

Coldfire Ejection Charge Ground Test

Before

Click here to play the higher resolution MPEG2 version of the video.

After

 

View High Resolution MPEG2 version of video

View QuickTime version of the video

View Low Res Windows Media Player version

Coldfire ejection charge testing showed that 3 grams of black powder was the right amount to use.

 

The proud owner of a brand new hybrid motor rocket!

Coldfire was completed in June 2007.

This page has been visited Hit Counter times.

Back to Top

 

 

 

 

 

  Home | What's New | Photos | Videos | Projects | Flight Data | Misc Info  | Links | Email

 

 

 All photos not otherwise credited were taken by Vern Knowles

Vern Knowles © 2002, 2003, 2004, 2005, 2006, 2007 All Rights Reserved