1. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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TEKNOFEST ROCKET CONTEST Preliminary Design Report (PDR) Presentation WARNING: Any format other than this Format is prohibited. It is forbidden to take any screenshots. Hand drawing prohibited. Care should be taken to prepare a completely professional presentation.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

2. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Structure of the Team
It is expected that a team will be formed in which team members are included in their roles in the team as well as university and university information.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

3. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Rocket General Design
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

4. Open Rocket General Design
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Open Rocket General Design
The overall design of the rocket should be taken from the open rocket file. The CAD design of the rocket must be reflected in the Open rocket as a whole.
The details of the size of a sub-system of the rocket such as Nose Cone, Electronic and Rescue Systems should be given.
An example flight profile should include:
Preparation of a table including Launch, Ramp, Burn Out, Apogee, Parachute Opening and Descent Speed, Altitude and Event Times. The visualization of the table will be evaluated as extra points.
Display the table as a visualized flight profile and determine the estimated drop point for wind speed of 10 m/s.
A time-dependent graph including speed, instantaneous acceleration, and altitude data, such as the sample chart specified in the next slide, must be created and added.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

5. Open Rocket General Design
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Open Rocket General Design
As can be obtained from Open Rocket, competitor teams can create graphs by themselves.
SAMPLE
SAMPLE
Sample Flight Profile Table
Time
Altitude
Speed
Launching T
Ramp Hill
T + t1 A Vr
Burn Out
T + t2 Y1
Vbr
Peak
T + t3 Y2 Va
Parachute Opening
T + t4 Y3 Vp
After Parachute - Vd
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

6. Mechanical Appearance & Mass Budget
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Mechanical Appearance & Mass Budget
General CAD design should be given. All parts of the rocket should be listed and their materials should be specified. Taking a general mass budget and placing it on the slide.
The details of the size of a sub-system of the rocket such as Nose Cone, Electronic and Recovery Systems should be given. Material and mechanical properties should be mentioned.
It should be which stated how the rocket will work in general.
This section should consist of at least 4 slides and should include CAD designs of all subsystems.
The details of the material selection, details and selection criteria which should be shared in this section.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

7. Mechanical Appearance & Mass Budget
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Mechanical Appearance & Mass Budget
Sample Mass Budget
Rocket Bill of Materials
Part Number
Component
Weight (Gram)
Material
Piece 1
Nose Cone Tip
0.8
Aluminum 2
Nose Cone Connection
0.155 3
Nose Cone
117
Carbon Fiber 4 5
Nose Cone Body
340 6
Eye Bolt Connection
1050
Steel 7
Eye Bolt 80
Forged Steel 8
Large Parachute 50
Ripstop Nylon 9
Extra Load
2000 - 10
Connection Part
139
SAMPLE
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

8. System Flight Analysis Datas
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System Flight Analysis Datas
The details of the values given in the Entry Report should be stated here.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

9. Operation Concept (CONOPS)
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Operation Concept (CONOPS)
The operational profile of the flight profile should be specified at what stage of the flight.
Instant data should be reported where the data will be stored.
Launch Process
Post-Launch Process and Recovery
Transport of the rocket to the ramp, loading the motor and how to do the ignition should be specified.
Strategies for the rescue team and the presence of the rocket should be specified.
SAMPLE
During the flight the rocket height chart
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

10. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Rocket Subsystems
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

11. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Nose Cone
Data such as height, geometry (Von Karman etc.), material and production method should be shared.
Production and test plans should be specified.
This section should not exceed two slides.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

12. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Recovery System
The decision should be explained comparatively. At least a different system should be indicated and its advantages and disadvantages should be indicated. The color of the system should be explained in detail.
The descent speed of the rocket should be explained as a summary (if any, with sample pictures) of how the system will exit and if it will be out of the rocket.
This section should not exceed two slides.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

13. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Avionics
A flight computer design should be provided to determine which sensors are to be received by the flight data of the rocket and to check the recovery systems. Adding control diagram will be evaluated as extra score.
All necessary tests and subsystems of the flight computer must be explained in detail. The sensors to be used, their functions and the relationship with other sensors / processors must be given in the control diagram.
This section should not exceed two slides.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

14. Structural – Body/Inside Body Structural Supports
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Body material and mechanical properties should be shared. (Internal mechanical structures should also be explained.)
The original production body should be explained with details of the production method. The mechanical properties of the structural materials must be resistant to the specified acceleration in the specification.
The tests to be performed in this respect should be specified and the strength properties of the materials should be indicated.
This section should not exceed two slides.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

15. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Structural - Fin
Fin material and mechanical properties should be shared. Wing design, geometry and structure should be determined.
The original production body should be explained with details of the production method.
This section should not exceed two slides.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

16. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Motor
The selected motor rocket compatibility and thrust time graph should be shared.
The assembly of the motor must be given in detail.
This part should not exceed 1 slide.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

17. Rocket Integration and Tests
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Rocket Integration and Tests
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

18. Rocket Integration Strategy
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Rocket Integration Strategy
Detailed information should be given on how to connect and interconnect all systems.
If the body consists of more than one structure, the connection mechanism should be explained.
This section should not exceed two slides.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

19. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Tests
The test schedule and test methods of all subsystems should be explained in detail.
Structural / mechanical strength tests,
Recovery Systems Separations
Nose Separations,
Avionic system tests,
Telecommunication tests (if any)
Tests should be indicated if there is any marshal mechanism.
This slide should not exceed at least 3 maximum 7 slides.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

20. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Calendar
Project calendar should be shared with details.
Recommendation: Using Microsoft Project is recommended.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)

21. 2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)
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Budget
All proposed materials and budget should be shared here.
January 9, 2019 Wednesday
2019 TEKNOFEST ROCKET CONTEST PRELIMINARY DESİGN REPORT (PDR)