Herkese Ak Public Team Logo TEKNOFEST 2020 ROCKET

Herkese Açık | Public Team Logo TEKNOFEST 2020 ROCKET CONTEST Preliminary Design Report (PDR) Presentation WARNING: It is not allowed to use any format other than this one. It is forbidden to take any screenshots. ( Graphics, data, code screenshot, Algorithm screen shots and CAD images can be included as long as they have high resolution and readability. However, it is forbidden to take any screen shots from any excel or word files. ) Hand drawings are not allowed. It is important to prepare a fully professional presentation. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 1

Herkese Açık | Public Team Structure Team Logo A scheme which includes team members’ university and faculty information, and their roles in the team is expected. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 2

Herkese Açık | Public Team Logo Rocket Basic Design 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 3

Herkese Açık | Public SUMMARY Team Logo General Information About Competition Rocket Length (metre): Diameter (metre): Rocket’s Dry Weight (kg. ): Propellant Weight (kg. ): Engine’s Dry Weight (kg. ): Payload Weight (kg. ): Total Take-off Weight (kg. ): Propulsion Type: Measurement Comment Expected Flight Data and Analysis Take-off Thrust/Weight Ratio: Ramp Speed(m/s): Minimum Static Balance Value During Combustion: Maximum acceleration (g): Maximum Speed(m/s & M): Calculated Altitude(m): 9 th March 2020, Monday Engine Choices Measurement Comment Brand : Cesaroni Name: Class: Engine’s Total Thrust Value(Ns): Name: Class: Teams should put their rocket’s information as a summary here. . Values here and the values in the Open Rocket file should be consistent. 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 4

Herkese Açık | Public Team Logo Open Rocket General Tasarım • Rocket’s general design should be taken from the open rocket file and added here. CAD designed rocket should be reflected to Open Rocket in exact ratios. • An example flight profile should include: • A table including Launch, Ramp, Burn Out, Apogee, Parachute Deployment and speed after parachute deployment, altitude and event times. A visualized version of the table should be evaluated as extra points. • Table visualized as a flight profile and an expected landing spot for 10 m/s wind speed hızı için belirlenlenmesi. (ONLY FOR THE FURTHEST LANDING SPOT)(IN SIMULATION the speed should be taken as 6 m/s ) • Like the example graphic in the next slide, a time dependent graphic including speed, instantaneous acceleration and altitude data should be created and added. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 5

Herkese Açık | Public Open Rocket General Design Team Logo Teams can create the graphics themselves or obtain the graphics from Open Rocket. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 6

Herkese Açık | Public Team Logo Mechanical Look & Weight Budget • General CAD design should be given. All rocket parts should be listed and predicted materials should be specified. General weight budget should be calculated and given in a slide. • Predicted sizes of every rocket subsystem such as nose cone, electronics, and recovery system should be given. • Rocket’s general behavior in every stage should be specified. • This part should have at least 4 slides and include general CAD views. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 7

Herkese Açık | Public Team Logo Mechanical Görünüm & Weight Budget Example weight budget 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 8

Herkese Açık | Public System Flight Analysis Data Team Logo Details about the values given in the fourth page should be specified here. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 9

Herkese Açık | Public Team Logo Operation Concept (CONOPS) Events during the flight should be specified over the flight profile. Teams should state how and where they will store their instantaneous data. – Launch Process – Post Launch Process and Recovery • Teams should state who will carry the rocket to the ramp, load the engine and launch and how they will do it. • Teams should state their recovery team and strategies for finding the rocket. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 10

Herkese Açık | Public Team Logo Roket Sub-Systems 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 11

Herkese Açık | Public Nose Cone Team Logo • Options for details like Length, Geometry (Von Karman etc. ), Material and production method should be considered and compared. Options’ advantages and disadvantages should be listed and options that are intended to be used before CDR should be declared with their reasons. • Expected production and test plans should be specified with their approximate date ranges. This should help forming a healthy schedule until CDR. • This part should not exceed 4 slides. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 12

Herkese Açık | Public Recovery System Team Logo • Planned recovery system should be explained with comparisons. At least more one system other than the planned system should be described with its advantages and disadvantages. The system’s colour and size should be explained in detail. Recovery strategy and stages should be specified. • Calculation of the rocket’s falling speed should be included. • If the system will leave the rocket, teams should summarize how it will leave the rocket and how it will be deployed (with photos if possible). • This part should not exceed two slides. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR)) 13

Herkese Açık | Public Avionics Team Logo • Teams should explain which sensors will be used to obtain flight data, and their planned flight computer design which will control recovery systems. Control diagrams will be evaluated as extra points. Different sensors should be compared and reasons for the planned sensors and systems should be explained. • Flight computer’s all planned test and sub-systems should be explained in general. Planned sensors, their functions and integration with other sensors/processors should be shown in the control diagram. • Systems and sensors that are planned to be in the rocket ( processor, sensor, actuator etc. ) should be compared with similar ones and reasons for deciding the planned parts should be explained. • System’s planned avionic system should be shown with a block diagram. This block diagram should include the cards that are planned to be in the system and systems’ connections. • Planned flight computer’s ( which will control the recovery systems ) design should be specified. Planned algorithm should be shown here with a flow diagram. • This part should not exceed two slides. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 14

Team Logo Structural – Body/Interior Structural Supports Herkese Açık | Public Different body material options and their mechanical properties should be shared (including internal system components) Reasons for choosing the proposed material should be explained in general. If it is an original production body, the production method options should be explained in detail. The tests that will be run on this subject should be stated in general. This part should not exceed two slides. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15

Herkese Açık | Public Structural - Fins Team Logo • Different fin material options and their mechanical properties should be shared. Reasons for choosing the proposed material should be explained in general. • Fin design, geometry and structure should be compared to other options and planned design criteria should be stated. • If it is an original production body, production method options should be explained in detail. • This part should not exceed two slides. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 16

Herkese Açık | Public Engine Team Logo • Chosen engine’s suitability to the rocket and assembly strategy should be shared. • Alternative options for the engine’s assembly strategy should be stated. Researches on this subject should be completed. Options’ advantages and disadvantages should be listed and reason for choosing the planned system should be pointed out. • This part should not exceed two slides. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 17

Herkese Açık | Public Team Logo Secondary Engine Choice • Planned minor modifications on the rocket for the secondary engine should be summarized. These changes should be explained with their reasons and it should be proved that the rocket fits criteria for the exit speed from the ramp and static margin after these changes. • Possible modifications can be changing systems’ places in the rocket, adding or subtracting weight, different fin choices, nose cone length and material options. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 18

Herkese Açık | Public Team Logo Rocket’s Assembly and Tests 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 19

Herkese Açık | Public Team Logo Rocket Assembly Strategy • Information about the options for connecting every system to each other should be given. • If the body consists of more than one structure, the connection mechanism options, and their advantages and disadvantages should be explained. • This part should not exceed two slides. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 20

Herkese Açık | Public Tests Team Logo • General test dates ( date range is sufficient ) for all sub-systems and intended test methods/options should be stated. • Structural/Mechanical strength tests, • Recovery system deployment tests, • Nose cone deployment tests, • Avionic system tests, • Telecommunication test ( if there any ) • This part should be at least 3 and at most 7 slides. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 21

Herkese Açık | Public Schedule Team Logo Project schedule should be shared in detail. Suggestion: Using Microsoft Project is recommended. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 22

Herkese Açık | Public Budget Team Logo All planned materials and budget should be shared here. 9 th March 2020, Monday 2020 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 23