Dust Devil High Altitude Project

 

by Frank De Brouwer TRA 06113 / Maverick 033

and Peter Muller TRA 09238 / Maverick 037


1.0 Introduction

In September 2008, Peter Muller and Frank De Brouwer flew some CanSats during ARLISS and some high altitude projects during XPRS in the BlackRock desert in the USA. During this launch an idea started to build a new project for a extreme altitude attempt.

While in BlackRock Desert enjoying the surroundings, the name for the rocket was born and it was to be Dust Devil as a result of the fine dust on the playa that creeps in everything.

The Dust Devil project members are Peter Muller and Frank De Brouwer under the flag of the Dutch Rocket Boys and the project is intended to fly in 2012, time schedule is mainly made by the funding and sponsors, construction is on track.

The European Altitude record (In Europe) lays around 12.5 Kilometers, the problem in Europe is that we have multiple rockets that can break this record easily, there is however no suitable launch site in Europe available to do this. In 2011 we aim to set the European Altitude record in the USA well above this 12.5 kilometers with Individual projects, and in 2012 we aim to set a very high altitude record in the USA with the Dust Devil. We aim for Space, but if this is possible remains to be seen and will be a result of the Pro150 motors that we can develop together with CTI for this project.

Sponsors;

Main Sponsors up till now are;

REBEL Space

To get this project in the air we are on the search of more sponsors. Please contact us for sponsor details and sponsor packages. Sponsor Letter can be found by clicking here. Sponsor Letter in Dutch can be found here. Contact information;

 

or

 

Individual Sponsors can contact us as we have a sponsor package in place for individual fliers. For a fee of 25 Euro we will fly your business card on this flight.

On the moment we are working on;

Designing the airframe in RockSim and Cad, REBEL Space is sponsoring the main airframe, the recovery and avionics, Performance Rocketry is sponsoring the first stage.

Designing the Pro150 motors for both stages with Jeroen Louwers from CTI (one with head end ignition). All 4 motors will be specially designed Pro150 motors with a Carbon Fiber Casing.

Designing a new high speed recovery system.

Designing the Avionics for this flight with GPS, downlink and a high resolution camera.

Getting the needed sponsors.

Setting up the infrastructure for shipping and the launch with Mavericks and the FAA as this is a class 3 rocket under the new regulations and Black Rock will be too small for this Rocket under the new regulations. We may opt for a European launch site, but this depends on funding as launching in Europe might be more expensive then in the USA.

Altitude predictions are now between 70 km (230.000 feet) and 120 km (400.000 feet or near Space) depending on the final airframe design and offcourse the design of the motors. Speed predictions are between Mach 3.1 and Mach 5.2

 

Contents Dust Devil Project

1.0 Introduction

2.0 Project Goals

3.0 Rocket Design

3.1 Pre-Flight Data Capture Form

3.2 Rock-Sim / CAD design

3.3 Materials

3.4 Motors

3.5 Avionics

3.6 Recovery

3.7 Flight Profile

4.0 Rocket Construction

4.1 First Stage

4.2 Second Stage

4.3 Motors

4.4 Avionics

4.5 Recovery

5.0 Flight

5.1 Launch Location

5.2 Pre Flight Checklist

5.3 Logistics

6.0 FAA Requirements

 

2.0 Project Goals

Lately amateur rocket builders have built more and more extreme projects that launch to high altitudes.

We as members of the Dutch Rocket Boys want to set the European High Altitude Amateur Rocket record on a higher level in. Our Flight with the Dust Devil is aimed on setting the European Amateur Altitude record to an unprecedented altitude, very close to Space, or just to nick it.

The highest verified altitude reached by a European built amateur rocket is 60.203 feet (18.350 meter) by a French Amateur group out of Paris who launched a rocket on the 13th of February 1998 from French Guyana. An Attempt to break this was done by the MARS Advanced Rocket Society out of the United Kingdom, who launched from the Black Rock Desert in October 2000, their rocket reached 34.579 feet (10.540 meter) and did not break the record. In March 2009 the group DARE from the TU Delft launched a rocket up to 41.010 feet (12.500 meter) from Kiruna in Sweden.

The Dutch Rocket Boys is a group of amateur rocket builders that design, fly and built allot of individual projects, which they launch in and outside of the Netherlands. The members are active members of Tripoli USA, Tripoli the Netherlands, United Kingdom Rocketry Organization and Mavericks in the United States.

We aim to launch this rocket close or into Space, with the main goal as doing this without support from a University, Records in Europe are limited by the lack of launch locations, that is why we opt for the USA. Designing and building the rocket will not be the hardest part, the hardest part will be to get launch permission and get the rocket there.

We will use newly developped motors that we will design together with CTI, the main reason for this is that we want dependable motors and the fact that building motors in Europe is impossible without very large investments for a project like this.

Basic Goals of this project;

Design, built, fly and recover a two stage 6 inch Carbon Fiber Rocket.

Design, built, fly and recover two research P motors with a total impulse of around 50.000 Nsec. per motor based on a revolutionary Carbon Fiber motor casing with solid fuel grains.

Design, built, fly and recover a reliable high-speed recovery system.

Launch and Recover the Rocket.

Set a European High Altitude Amateur overall high altitude record around 100 kilometers.

Film the curvature of the earth during the flight.

3.0 Rocket Design

3.1 Pre-Flight Data Capture Form

Name

Peter Muller - Frank De Brouwer

TRA 09238 - 06113

Launch Location

To be determined

Date

2012

Rocket Source

Modified Performance Rocketry Mongoose

Rocket Name

Dust Devil

Colors

White, Grey, Silver, Black

Rocket Diameter

6 inch

Rocket Length

over 6 meter

Rocket Weight Loaded

To be determined

Avionics Description

4 tiny RDAS with GPS / UFC2 or 3

Motor Type

CTI Pro150 Motors with Carbon Fiber Casings

Thrust to weight Ratio

To be determined

Launcher requirements

To be determined

Length

To be determined

CP

To be determined

How calculated

To be determined

CG

To be determined

How calculated

To be determined

Maximum Velocity

To be determined

How calculated

To be determined

Maximum altitude

To be determined

How calculated

To be determined

 

3.2 Rock-Sim / CAD design

Under development

We made the basic design in RockSim 9.0, after this we made a CAD drawing of the rocket to be able to manufacture the special parts and to convert this drawing for use in a CFD package.

3.3 Materials

F181 Dust Devil

Parts

Project Designation

Material

Performance Mongoose 150

Aluminum Tip

Nose Cone

Aluminum

Composite 5:1 Conical Nose Cone

Nose Cone

Composite

Carbon Fiber Nose Cone Bulk Plate 1/4"

Nose Cone

Carbon Fiber

Filament Wound Carbon Fiber Airframe 48"

Avionics / Recovery

Carbon Fiber

Filament Wound Carbon Fiber Coupler 16"

Coupler / Avionics

Carbon Fiber

2 Aluminum REBEL Avionics Bay Bulk Plates

Coupler / Avionics

Aluminum

2 Aluminum Avionics Bay Sleds

Coupler / Avionics

Aluminum

2 Aluminum Avionics Bay Sleds

Coupler / Avionics

Aluminum

Filament Wound Carbon Fiber Airframe 64"

Sustainer Stage

Carbon Fiber

Carbon Fiber Fins 1/4" Beveled

Sustainer Fins

Carbon Fiber

High Temp Epoxy (500F-260C)

Epoxy

Epoxy

Inter Stage Coupler

Aluminum CNC Coupler

Inter Stage Coupler

Aluminum

Performance Mongoose 150 Booster Special Design

6 Aluminum REBEL Avionics Bay Bulk Plates

Booster / Avionics

Aluminum

3 Aluminum Avionics Bay Sleds

Booster / Avionics

Aluminum

3 Motor Retention Rod with Eye Bolt

Booster / Avionics

Stainless Steel

3 Filament Wound Carbon Fiber Coupler 8"

Booster / Avionics

Carbon Fiber

3 Filament Wound Carbon Fiber Airframe 64"

Booster Stage

Carbon Fiber

3 Carbon Fiber Fins 1/4" Beveled

Booster Fins

Carbon Fiber

High Temp Epoxy (500F-260C)

Epoxy

Epoxy

Motors

Booster 3 Motors

Performance Carbon Casing

Booster Motor

Carbon Fiber

Forward Closure

Booster Motor

Aluminum / G10

Liner

Booster Motor

Phenolic

Grains

Booster Motor

AP

Aft Closure

Booster Motor

Aluminum / G10

Graphite Nozzle

Booster Motor

Graphite

Igniter

Booster Motor

Wire

Sustainer

Performance Carbon Casing

Sustainer Motor

Carbon Fiber

Forward Closure

Sustainer Motor

Aluminum / G10

Liner

Sustainer Motor

Phenolic

Grains

Sustainer Motor

AP

Aft Closure

Sustainer Motor

Aluminum / G10

Graphite Nozzle

Sustainer Motor

Graphite

Igniter

Sustainer Motor

Wire

Recovery

Sustainer Drogue Chute and Streamer

Sustainer Recovery

Rip Stop Nylon

Sustainer Main Chute

Sustainer Recovery

Rip Stop Nylon

Sustainer Lines

Sustainer Recovery

Kevlar

Booster Drogue Chute and Streamer

Booster Recovery

Rip Stop Nylon

Booster Main Chute

Booster Recovery

Rip Stop Nylon

Booster Lines

Booster Recovery

Kevlar

Avionics

High End Camera with lens on outside

Nose Cone Avionics

Electronics

BMMW UFC2

Nose Cone Avionics

Electronics

2 tiny RDAS with GPS and Downlink

Sustainer Avionics

Electronics

2 tiny RDAS

Booster Avionics

Electronics

Launcher

8mm or larger railguides

Guidance

Stainless Steel

Carbon Coupler parts for attachment

Guidance

Carbon Fiber


3.4 Motors

3.5 Avionics

Basic setup;

Nose Avionics Section;

High End Camera; Filming of the curvature of the Earth.

BMMW UFC2; DATA Gathering, GPS and downlink.

Sustainer Section;

2 tiny RDAS with GPS, Downlink and Orientation;

Orientation decision for ignition of 2nd stage;
Activation of double Rouse CO2 system for Drogue Chute Deployment;
Activation of fail safe Release mechanism (ARRD and Tether) for Main Chute Deployment.

Booster Avionics Section;

2 tiny RDAS;

Activation of 2 BP charges for Drogue Streamer Deployment;
Activation of fail safe Release Mechanism (ARRD and Tether) for Main Chute Deployment.

3.6 Recovery

3.7 Flight Profile

4.0 Rocket Construction

4.1 First Stage

4.2 Second Stage

20090318The first parts from Performance Rocketry have arrived.

More Parts in the REBEL Space workshop

The second stage is ready for paint

4.3 Motors

4.4 Avionics

4.5 Recovery

5.0 Flight

5.1 Launch Location

5.2 Pre Flight Checklist

 

5.3 Logistics

The rocket will ship in parts with the needed tools in a crate. After the launch the Rockets will be re packed and send back to Europe.

As we had some major US Customs delaysin 2008 we will now ship earlier to prevent delays or cancellation of the launch.

6.0 FAA Requirements

When a Class 3 - Advanced High-Power Rocket requires a certificate of waiver or authorization the person planning the operation must provide the information below for each type of rocket to the FAA at least 45 days before the proposed operation. The FAA may request additional information if necessary to ensure the proposed operations can be safely conducted. The information shall include for each type of Class 3 rocket expected to be flown:

(1) The information requirements of paragraph (a) of this section*.
(2) Maximum possible range,
(3) The dynamic stability characteristics for the entire flight profile,
(4) A description of all major rocket systems, including structural, pneumatic, propellant, propulsion, ignition, electrical, avionics, recovery, wind-weighting, flight control, and tracking,
(5) A description of other support equipment necessary for a safe operation,
(6) The planned flight profile and sequence of events,
(7) All nominal impact areas, including those for any spent motors and other discarded hardware, within three standard deviations of the mean impact point,
(8) Launch commit criteria,
(9) Countdown procedures, and
(10) Mishap procedures.

* Paragraph (a) requirements:
(1) Estimated number of rockets,
(2) Type of propulsion (liquid or solid), fuel(s) and oxidizer(s),
(3) Description of the launcher(s) planned to be used, including any airborne platform(s),
(4) Description of recovery system,
(5) Highest altitude, above ground level, expected to be reached,
(6) Launch site latitude, longitude, and elevation, and
(7) Any additional safety procedures that will be followed.