Requirements for Rocket Competition Preliminary Design Report
The Rocket Competition Preliminary Design Report specifies strict guidelines including font size, font type, formatting, referencing, and content organization. Adherence to these requirements is crucial to avoid point deductions or disqualification. Plagiarism is strictly prohibited, and visuals and data must be appropriately referenced. Detailed information on tables, charts, and text presentation is provided to ensure clarity and compliance with the specified standards.
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Herkese Ak | Public WARNING For the entire report, the minimum font size must be 18 and the font must be Calibri, without exception. Paragraphs must not be bold or highlighted. The margins of the report template must be respected. If the information requested in the report is not included in the relevant section, this will be deducted from the score (Including the information in another part of the report does not count). If the requested information is not included in the corresponding slide, the relevant team will be disqualified in accordance with the disqualification criteria. Any cited information must be referenced. The reference may be at the bottom of each slide, or they may be collectively presented with numbering in a reference slide at the end of the report. Teams found to have plagiarized the works of others shall be disqualified. Visuals, such as tables, schemes, equations, etc. are also to be referenced. Shared dimensions must be presented using visuals that comply with the technical drawing format. All units in the report must be specified in accordance with the International System of Units. Measurements with missing units will not be taken into consideration. The tables used must not be different from the table format in the relevant slide. Charts and tables must be titled. Untitled charts and tables will not be taken into consideration. The charts and tables should be presented in similar sizes to those in the template. The information on the systems should be concise and easily understandable (clear). Tables and visuals should be utilized where needed for materials, sizing, comparisons, etc. The text colour of the element selected in a comparison should be green. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 1
Herkese Ak | Public WARNING Information requested more than once throughout the report must be specified separately on each slide where requested. Even if the missing information has been provided in a previous slide, it will be deducted from scoring if absent, or if necessary, the team will be disqualified. The names of the documents (including tables) that are requested or permitted in the Annex must be included on the relevant slide, and the documents must be submitted in full, together with the PDR. Screenshots of tables should not be provided when presenting the tables to be presented in PDR or its Annex. The texts, formulas, equations (the Powerpoint formula and equation editor should be used), correlations etc. to be presented in the PDR or its Annex should not be presented in the form of a screenshot. The logo must be on every page of the report, and the titles must not be changed for any reason. No new and/or different slide should be added to the slides in the template shared by the Competition Committee. The report must be uploaded in PDF format. Reports submitted in a format other than PDF shall not be evaluated under any circumstances. Even if not specifically stated in the articles above, information that is not provided in accordance with the PDR format shall not be evaluated. Texts (including specification articles), sample images and boxes on the slides that are included to guide the competitors must be deleted. AFTER THE WARNING PAGE HAS BEEN READ, IT MUST BE DELETED, AND MUST NOT BE INCLUDED IN THE REPORT. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 2
Herkese Ak | Public Team Logo TEKNOFEST 2024 ROCKET COMPETITION Challenging Task Category Preliminary Design Report (PDR) Presentation Team Name 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 3
Herkese Ak | Public Team Structure Team Logo A chart is to be created presenting the education status of the team members, their departments, their University and institution information, as well as their roles within the team. If there are foreign national competitors, this should be specifically reported. This section must not exceed 1 (one) slide. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 4
Competing Rocket General Information Herkese A k | Public Team Logo Predicted Flight Data and Analyses General Information About the Competing Rocket Measure Measure Takeoff Thrust to Weight Ratio: Rail Exit Velocity (m/s): Stability (for Mach 0.3): Maximum acceleration (g): Maximum Velocity (m/s): Highest Mach Number: Apogee (m): Height (mm): Diameter (mm): Dry Weight of the Rocket (g): Fuel Mass (g): Dry Weight of Engine (g): Payload Weight (g): Total Takeoff Weight (g): Engine The summary information of the rocket must be given in the table. The values in the Open Rocket file and the values typed here must be consistent. This box must be deleted. Engine Name 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 5
Herkese Ak | Public General Design Team Logo The visual should include the static margin, length and height of each functional part of the rocket. The CAD-designed rocket must be reflected on Open Rocket at a 1:1 scale. The enlarged visuals of the upper left corner containing Height- Mass-Diameter information, the upper right corner containing Stability-CG-CP information, and the lower left corner containing Apogee-MaxVel-MaxAcc information (as shown in the visual below), taken from the Open Rocket screenshot, should be also included outside the visual. No new table should be made. An exact replica of the visual must be prepared. The size of each part should be included, as in the sample visual below. Like in the visual, each section should be referenced with lines drawn outward, the section names should be written, and the sizes should be provided. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 6
Herkese Ak | Public Operation Concept (CONOPS) Team Logo The flight profile should be provided visually, and which action will be performed operationally at what stage of the flight should be indicated on this visual. All processes should be included, from the moment of the ignition of the rocket to its recovery, in sequence. Hand drawings are prohibited. Stages are to be numbered in the visual. Each stage is to be explained as in the example given below (Sample Flight Profile Table) In the same flight profile, the stage and the manner in which the "Mission Payload" leaves the rocket are to be specified, as well as the flight profile. This section must not exceed 1 (one) slide. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 7
Herkese Ak | Public Flight Simulation Report (FSR) Team Logo Flight Simulation Reports are not a disqualification criterion for the Challenging Mission Category, but are scored. The Flight Simulation Reports prepared by the teams will be uploaded separately to the system, along with the PDR. The FSR will not be shared in PDR. This Page will be left blank. The name of the report uploaded in PDF format should be specified here. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 8
Herkese Ak | Public Mass Budget Team Logo A product tree spreadsheet including all parts of the rocket will be prepared to resemble the example in the slide, and uploaded onto the system as a separate file. Sample Mass Budget 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 9
Herkese Ak | Public Team Logo Rocket Subsystem Details 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 10
Herkese Ak | Public Trade-off Analysis Table Team Logo The features of each subsystem in the report are to be written under sub-headings, as indicated in the table. Teams are expected to perform trade-off analysis by making detailed advantage/disadvantage comparisons of the options they have at hand with regards to system features. This page is an example. The table is indicated for use in other slides. The information on this slide is not expected. After the table has been taken, it must be deleted. Trade-off Analysis Table Option 1 Option 2 Feature Trade-off Analysis Explanation Factor Advantage Disadvantage Factor Advantage Disadvantage Linear Actuated Separation System Hard to manufacture. High cost. Easy to manufacture. Low cost. Rather than a CO2 tube separation system, a Linear Actuated separation system has been preferred as it is easier to manufacture and is lower in cost. Design/Operation Principle CO2 Tube Separation System .. .. The usage of Aluminium in the design of the relevant system increases the manufacturability of the design. At the same time, the usage of aluminium as a material Material Carbon fibre .. .. Aluminium .. .. Method of Manufacture Hand Lay-up .. .. Machining .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 11
Herkese Ak | Public Nose Cone Detail Team Logo The table and concept design CAD visual specified in the tenth slide must be presented here. Details of the nose cone design (selected geometry, shape coefficient, etc.) are to be shared. This part must not exceed 2 (two) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 12
Herkese Ak | Public Fin Detail Team Logo The table and concept design CAD visual specified in the tenth slide must be presented here. Details of the fin design (the root & tip length, angles etc. of the fin) are to be shared. This part must not exceed 2 (two) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 13
Frame and Integration Parts (STRUCTURAL) Mechanical View Herkese A k | Public Team Logo The table and concept design CAD visual specified in the tenth slide must be presented here. Frame lengths and diameters must be shared. This part must not exceed 3 (three) slides. * The parts that are mechanically accessible from outside should also be presented, with details. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 14
Herkese Ak | Public Team Logo Stage Separation System Mechanical View 3D View of the Stage Separation System (CAD) The "basic level" CAD outputs of the system that is planned for use used must be shared in such a way that the components that make up the subsystem can be understood in detail. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 15
Herkese Ak | Public Stage Separation System Team Logo The size of the system, and how the stage is to separate from the system chosen must be explained at the basiclevel . The working principle of the system that is planned for use should be explained step-by-step, with the support of basiclevel CAD visuals. All elements used in the planned system should be explained one-by-one, along with their functions. In the planned system, the suitability of the rocket for the operating conditions at the given altitude should be explained. (Especially in Pneumatic & Hydraulic System Designs, it should be shown that the design is made considering basically the altitude at which the stage separation system is located). An explanation should be given about the connection strategy of the stage separation system to the rocket. (Moment and load analyses of the planned connection points should be shown at a basiclevel and appropriate connection options/elements should be explained.) The timing of every event in the stage separation, and the reasoning for the timing of each event must be explained. The reasoning behind the timing planning criteria should be explained at a basiclevel . This part must not exceed 5 (five) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 16
Engine Compartment Mechanical View & Detail Herkese A k | Public Team Logo The table and concept design CAD visual specified in the tenth slide must be presented here. It should be explained and proven with visuals that the engines are installed on the rocket last in the assembly sequence. For the installation strategy of the engines, a trade-off analysis should be carried out and the options should be explained. This section must not exceed 2 (two) slides. 3D View of Engine Compartment (CAD) 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 17
Herkese Ak | Public Analyses Team Logo The analysis schedule and analysis methods of all subsystems must be explained in detail. The projected analysis methods must be specified. The analysis schedule and details of the analyses should be specified on separate presentation pages, by including the parts specified below. 1st Section: Analysis Schedule: In this section, the teams are expected to share a schedule specifying when they will carry out the analyses they have planned to do. Sharing of this schedule is mandatory. This part must not exceed 2 (two) slides. 2. Section: Structural/Mechanical Endurance Analysis: In this section, the teams are expected to share the Structural/Mechanical Endurance Analysis they plan to carry out on their systems. Teams are expected to share a detailed plan of the analyses they expect to perform. Sharing the Analyses of Structural/Mechanical Endurance is mandatory. This part must not exceed 2 (two) slides. 3. Section: Computational Fluid Dynamics Analyses: In this section, the teams are expected to share the Computational Fluid Dynamics Analysis that they envision for their systems. Teams are expected to share a detailed plan of the analyses they expect to perform. Sharing the Computational Fluid Dynamics Analyses is mandatory. This part must not exceed 2 (two) slides. Any specific analyses should also be shared, along with justification. All analyses should be designed to provide information that addresses the following points: The program planned for use in the analysis. The planned analysis method. The data planned to be obtained from the analysis. How this data will be interpreted. In PDR, the teams are expected to share their plans for the analyses. This is mandatory. The results of these planned analyses will be shared in the CDR. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 18
Recovery System - Parachute Deployment System Herkese A k | Public Team Logo Recovery systems that can be used in the design must be compared in terms of their advantages and disadvantages. The system decided must be explained and the reasoning must be given. The table and concept design CAD visual specified in the tenth slide must be presented here. The recovery strategy and stages are to be specified. (The system that will activate the recovery system is to be described with details.) The functions aboard the rocket of the recovery subsystem parts are to be described. Information about the volume that the recovery system will occupy in the rocket is to be shared. This part must not exceed 3 (three) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 19
Hot Gas Generator Requirements Herkese A k | Public Team Logo This section is to be filled in only by teams wishing to perform rocket separation using pyrotechnic material. Teams that do not use pyrotechnic materials are obliged to clearly state on this page that they do not use pyrotechnic materials. In accordance with Articles 3.2.2.2.10, 3.2.2.2.11 and 3.2.2.2.12 of the Specifications: 3.2.2.10. The teams will not be allowed to use their own pyrotechnic material in their hot gas generator systems. 3.2.2.11. The pyrotechnic hot gas generator (in capsule form) will be hand-delivered by the TEKNOFEST Rocket Competition Committee to the teams that will use the Hot Gas Generator (HGU) in the launch site, and information about the HGU is given in Annex 3. 3.2.2.12. During the installation/integration activities in the Aksaray Launch Site, the teams must prove that the hot gas generator provided by the TEKNOFEST Rocket Competition Committee is used in the rocket. Otherwise, they will be eliminated. The teams that will use the hot gas generators in question are required to fill in the table below based on their preliminary designs. Separation Volumetric diameter to be pressurised (mm) Volume to be pressurised (m^3) Pressure to be reached (Bar) 1st Separation 2. Separation (If any) 3. Separation (If any) 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 20
Herkese Ak | Public Recovery System - Parachutes -1 Team Logo The colour and size of the parachutes must be explained in detail. Blue, white and grey colours must not be selected. Parachutes that are red, burgundy, brown or orange should be preferred. The rocket's terminal velocity calculations and parachute design are to be summarized. It should be demonstrated that the terminal velocities with parachute are in accordance with the specifications. Information on the parachutes must be given in table form. Information such as terminal velocity, colour, dimensions (folded-deployed) and mass must be specified. The GPS, radio signal transmitter and sensors if any on each item to be recovered must be presented separately for each item. This part must not exceed 3 (three) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 21
Herkese Ak | Public Recovery System - Parachutes -2 Team Logo The compliance of the parachute terminal velocities with the specifications will be checked with the table below. The table below must be filled in correctly and completely. Teams whose terminal velocities do not comply with the specifications will be disqualified. The terminal velocity for the secondary parachute should be calculated taking into account that the primary and secondary parachute will be used together. Parachute System (m^2) by the parachute system (kg) Parachute Area Mass to be carried Parachute Drag Coefficient Terminal Velocity (m/s) Primary Parachute Secondary Parachute Stage Parachute Payload Parachute 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 22
Herkese Ak | Public Payload Team Logo (IF ANY) The function of the payload must be described and a draft CAD visual must be provided to share the overall dimensions of the payload. How the payload will be separated from the rocket must be explained. The stage, the manner of separation and the location process afterwards must be explained. A positioning system must be included to allow the recovery of the payload. The positioning system on the payload must be described in detail. The payload mass must be shared. This part must not exceed 2 (two) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 23
Herkese Ak | Public Avionics Summary Team Logo be used in the category Group A must be a commercial FCC. Otherwise, the team will be eliminated. 3.2.6.3 The commercial FCCs that the teams will use must be selected from among the products listed in Annex 5 (products approved by the TEKNOFEST Rocket Competition Committee). Otherwise, the team will be eliminated. The Flight Control Computers that are planned for use must be introduced in this slide. In Medium- and High-Altitude and Challenging Mission Categories, one (1) of the flight control computers must be indigenously developed. In Medium- and High-Altitude and Challenging Mission Categories, the second flight control computer must be a commercial flight control computer. Each commercial and indigenously developed system in the system should be listed and its main tasks should be written. For commercial systems, the full name and code of the product must be shared. The similarities and differences of the two flight control computers planned for use must be presented with a summary table. The means of switching between two flight control computers must be explained at a basic level. Any links between the flight control computers must be explained in detail. This part must not exceed 2 (two) slides. In accordance with the following articles of the Specifications: 3.2.6.1. The separation and recovery systems on the rocket are managed by the flight control computer (FCC). 3.2.6.2 Although the number of FCCs to be used in the rocket varies depending on the category, one of the FCC to 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 24
Herkese Ak | Public Avionics System 1 Detail/1 Team Logo The selection criteria for the basic circuit elements (Sensor, Controller and/or processors) used in the first flight control computer must be shared, and their advantages and disadvantages must be presented in the table. The functions of the elements within the circuit should be described briefly in the explanation section. Both the type (barometer, GPS, processor, etc.) and code should be specified when specifying circuit elements. Elements that are planned for selection must be highlighted in green. This part must not exceed 2 (two) slides. Name Code Advantage Disadvantage Explanation Y Barometer YYYY High precision Low frequency sampling X GPS XXXX . . Z Processor ZZZZ . . . . . . . . . . 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 25
Herkese Ak | Public Avionics System 1 Detail/2 Team Logo The circuit block diagram showing the structure of the first flight control computer must be shared. In this block diagram, all connections between the cards themselves as well as systems and cards should be visible. A flight computer board design that includes the sensors, controllers/processors and circuit elements used in the system must be shared at a basic level. This part must not exceed 2 (two) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 26
Herkese Ak | Public Avionics System 1 Detail/3 Team Logo 1st The recovery system algorithm to be used in the second avionics system should be shared at a basic level. 1st The parameters that will trigger the recovery system should be listed on the slide and the reasoning for their selection should be explained. The data to be filtered by planned data filtering methods must be explained, along with the reasoning behind the data filtering method selection. If the system used is a commercial system, the settings to be made while using the system must be mentioned on this page. This part must not exceed 2 (two) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 27
Herkese Ak | Public Avionics System 2 Detail/1 Team Logo The selection criteria of the basic circuit elements (Sensor, Controller and/or processors) used in the second flight control computer must be shared, and their advantages and disadvantages must be indicated in the table. The functions of the elements within the circuit should be described briefly in the explanation section. Both the type (barometer, GPS, processor, etc.) and code should be specified when specifying circuit elements. Elements that are planned for selection must be highlighted in green. This part must not exceed 2 (two) slides. Name Code Advantage Disadvantage Explanation Y Barometer YYYY High precision Low frequency sampling X GPS XXXX . . Z Processor ZZZZ . . . . . . . . . . 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 28
Herkese Ak | Public Avionics System 2 Detail/2 Team Logo The circuit block diagram showing the structure of the second flight control computer must be shared. In this block diagram, all connections between the cards themselves as well as systems and cards should be visible. A flight computer board design that includes the sensors, controllers/processors and circuit elements used in the system must be shared at a basic level. This part must not exceed 2 (two) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 29
Herkese Ak | Public Avionics System 2 Detail/3 Team Logo 2. The recovery system algorithm to be used in the second avionics system should be shared at a basic level. 1st The parameters that will trigger the recovery system should be listed on the slide and the reasoning for their selection should be explained. The data to be filtered by planned data filtering methods must be explained, along with the reasoning behind the data filtering method selection. If a commercial system is used, the settings to be made while using the system must be mentioned on this page. This part must not exceed 2 (two) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 30
Herkese Ak | Public Avionics/EOU Team Logo In accordance with the competition specifications: 3.2.9.12. An Electronic Observation Unit (EOU) was developed by the TEKNOFEST Rocket Competition Committee to ensure safe stage separation in the air. 3.2.9.13. The EOU contains electronic hardware, sensors and a power supply, and has mechanical integrity. 3.2.9.14. EOU allows the ignition of the second stage engine after checking whether the stage separation has occurred and whether the second stage is in the appropriate position. 3.2.9.15. The components, operating conditions, and the mechanical (size envelope, mass, etc.) and electrical (connection interfaces, etc.) features of the EOU are given in Annex 8. 3.2.9.16. The EOU will observe the stage separation with the working principle detailed in ANNEX-8. (The procedures the teams need to carry out for their designs are also given in Annex 8). 3.2.9.17. Teams will be able to use the EOU in the stage separation of their rockets. 3.2.9.18. Teams that do not use the EOU will develop their own measures to safely perform stage separation and prove their measures in the relevant reports (PDR, CDR and LLR). Teams using the EOU are required to generate a second stage ignition signal and transfer the data read to the avionics of the competing teams. The competitors will also be required to transfer this data as a package to their ground stations. A block diagram should be provided at basic level to describe the control algorithm of this process, which will take place from the triggering of the stage separation system until the termination of the communication between the EOU and the main avionic system. It must be demonstrated that the number of CONTROL CRITERIA used in the algorithm provided on the Avionics Detail/3 slide is at least 3; and the reasoning for the selection of these criteria must be explained. The options of how to establish a connection between the flight computer and the stage separation system, and how the wiring will be made, should be explained in detail. How the sensor data will be filtered should be explained This part must not exceed 3 (three) slides. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 31
Herkese Ak | Public Avionics Communication Team Logo Information must be provided about the modules that are planned to be selected for communication, and the selection criteria. It must be clearly stated which data will be transmitted to the ground station. The band and the data packet type of the data transmission must be specified. This part must not exceed 1 (one) slide. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 32
Herkese Ak | Public Budget Team Logo The cost and production budget information of all projected subsystem parts must be shared here. This part must not exceed 1 (one) slide. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 33
Herkese Ak | Public Checklist Team Logo This section should include a checklist for the control of whether all the requirements in the specification have been met. The part of the PDR in which these requirements are provided and the method of meeting the requirements (technical drawing, analysis, test, etc.) should also be specified. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 34
FMEA Herkese A k | Public Team Logo Failure Modes and Effects Analysis A Failure Modes and Effects Analysis (FMEA) should be included in this section. 2024 TEKNOFEST ROCKET COMPETITION PRELIMINARY DESIGN REPORT (PDR) 15 January 2024, Monday 35
