ARI CANSAT TEAM. France Cansat Competition February 2011
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1 ARI CANSAT TEAM ARIC-1 Preliminary Design Review France Cansat Competition p February 2011
2 Team Organization Sajjad Ghazanfarinia, System Design, Team Leader Hooman Jazebizadeh, System Design Sahar Bakhtiari, Aerospace Engineering g Mohammadreza Simard, Electrical Engineering Ghazale Ahmadi, Recovery Samane Tadayyon, Recovery
3 Mission Objectives Atmospheric Data Collection During Flight Deployment of Antenna at Ground Touch Real-Time Data Transmission
4 Concept of Operations PreFlight Briefing Launch and Release Recovery and Data Transmission to Ground Station Dimension and RF Check Launch System Integration Locate and Recover Cansat At the Launch Flight Site Preparation Prepare and Present PFR Team Activity Before Launch Cansat Operation Team Activity After Launch
5 System Functional Requirements & Physical s SYS-01 Cansat Mass Shall be Under 350gr. Competition Structure High I SYS-02 Cansat Dimensions Shall Fit Standard Soda Can. (r66,h115) Competition Structure High I SYS-03 Cansat Shall be Compatible with Launch System. Competition Structure,Recovry High I SYS-04 Cansat Shall Land on Ground Safely. Mission Recovery Medium T SYS-05 Cansat Materials Shall be Unharmful. Competition Structure Medium I SYS-06 Cansat Shall Obey Telecommunication Regulations. Competition Communication High A,D SYS-07 Cansat Shall Sound Atmospheric Parameters. Mission Payload High T SYS-08 Cansat Shall Collect Data Related to Sounding Sensors. Mission OBDH High D SYS-09 Cansat Shall Transmit GPS, Sensors and HK data. Mission Communication Medium D,T SYS-10 Cansat Cost Shall be Under 500. Funding - Low I,A SYS-11 Cansat Shall Remain Operational for 90 (TBC) Minutes. CONOPS Power Low A,T SYS-12 Cansat Shall Resist Operation Loads. CONOPS Structure Medium A,T SYS-13 Cansat Shall Deploy an Antenna at Landing. Mission Payload High T
6 Subsystems Payloads Onboard Computer Communication Power Recovery Structure
7 Payload-1 Function: Atmospheric Sounding Requirements PAY-01 Payload-1 Shall Sound Air Temperature, Pressure and Humidity. SYS-07 Sensors High D,T PAY-02 Payload-1 Shall Provide GPS Location. SYS-07 GPS Receiver High D,T PAY-03 Payload-1 Shall Acceleration Profile during Operation. SYS-07 Accelerometer Medium D,T PAY-04 Payload-1 Shall Support Sensors for Electronic Connections. SYS-07 Electronic Boards High T PAY-05 Payload-1 Mass Shall be Under 60 grams. SYS-01 Payload-1 High I PAY-06 Payload-1 Power Consumption Shall be Under 150mW. SYS-11 Payload-1 Medium T Elements: Sensors for Temperature and Humidity (SHT10), Pressure (MPX6300) and Acceleration (ADXL303), and GPS (GT723).
8 Payload-2 Function: Antenna Deployment Requirements PAY-07 Payload-2 Shall Sense Landing Instance. SYS-12 GPS Receiver High D,T PAY-08 Payload-2 Shall Deploy an Antenna at Landing. SYS-12 PAY-09 Payload-2 Shall Deploy Antenna with OBC Command. SYS-12 Deployment Mechanism Deployment Mechanism High Medium PAY-11 Payload-2 Mass Shall be Under 55 grams. SYS-01 Payload-2 High I PAY-12 Payload-2 Power Consumption Shall be Under 150mW. SYS-11 Payload-2 Medium T D,T D,T Elements Accelerometer (ADXL303), Spring Antenna, Deployment Mechanism
9 Onboard Computer Function: Data and Command Handling Requirements OBC-01 OBC Shall Collect Data from Sensors and GPS. SYS-08 Electrical Boards High T OBC-02 OBC Shall Save Data in Packages on a Memory during Mission. Mission Memory Medium T OBC-03 OBC Shall Make Data Packages Ready for Transmitting. SYS-09 Microprocessor High T OBC-04 OBC Shall Send Data Package to COM. SYS-09 Microprocessor High T OBC-05 OBC Shall Command Antenna Deployment. SYS-12 Microprocessor High T OBC-06 OBC Mass Shall be Under 30 grams. SYS-01 OBC High I OBC-07 OBC Power Consumption Shall be Under 50mW. SYS-11 OBC Medium T Elements Microprocessor (ATMega8) and Connectors
10 Communication Function: Data Transmission Requirements COM-01 COM Shall Transmit Data Packages to Ground Station. SYS-09 Transmitter High T COM-02 COM Shall Obey Competition Regulation for Transmit Frequency. SYS-06 Transmitter, Antenna High AT A,T COM-03 COM Shall Obey Competition Regulations for Transmit Power. SYS-06 Transmitter High A,T COM-04 Antenna Shall Fit in Cansat Size During Launch Phase. SYS-02 Antenna High A,T COM-05 Transmitter Shall Support 150 meters of Range. Competition Transmitter High A,T COM-06 COM Mass Shall be Under 40 grams. SYS-01 COM High I COM-07 COM Power Consumption Shall be Under 100mW. SYS-11 COM Medium T Elements Transceiver (RXQ2), Antenna
11 Power Function: Electrical Energy Supply Requirements: EPS-01 EPS Shall Support Voltage of all Parts. Mission Regulators, Battery High T EPS-02 EPS Shall Support Needed Current of all Parts. Mission Regulators, Battery High T EPS-03 EPS Shall Support System with Power for 90 (TBC) Minutes. SYS-11 Battery Medium T EPS-04 EPS Shall Provide On/Off Mode for System. Competition Switch High D EPS-05 Battery Shall be Replaceable. - Connectors Medium D EPS-06 EPS Mass Shall be Under 50 grams. SYS-01 EPS High I EPS-07 EPS Power Consumption Shall be Under 30mW. SYS-11 EPS Medium T Elements: Battery, Regulators, Switch and Connectors
12 Recovery Function: Returning in a Safe Flight Requirements: RCV-01 RCV Shall Operate Automatically and Passive. Mission Packing High T RCV-02 RCV Shall Make System to Descend Lower than 5mps. SYS-04 Parachute High A,T RCV-03 RCV Shall Fit Soda Can Size other than Cansat During Launch. SYS-02 RCV High I RCV-04 RCV Shall Resist Deployment Loads. SYS-12 Parachute and Fixture High T RCV-05 RCV Material Shall be Unharmful. SYS-05 Parachute Fabric Medium I RCV-06 RCV Mass Shall be Under 55 grams. SYS-01 RCV High I Elements: Parachute, Fixture
13 Structure Function: Providing Fixture and Shape of Parts Requirements: STR-01 STR Shall Fit Soda Can Size. SYS-02 STR High I STR-02 STR Shall be Compatible with Launch System. SYS-03 STR High I,T STR-03 STR Shall Resist all Operational Loads. SYS-12 Material High T STR-04 STR Shall Resist Crash Loads in case of RCV Failure. Mission STR Medium T STR-05 STR Material Shall be Unharmful. SYS-05 Material Medium I STR-06 STR Mass Shall be Under 60 grams. SYS-01 STR High I Elements: Frame Rods, Casing
14 Ground Station Function: Display of Cansat Results Requirements: GSE-01 GS Shall Provide a HW Compatible with Cansat. Mission GS HW Medium T GSE-02 GS Shall Provide an Interface with Computer. Mission GS HW Medium T GSE-03 GS Shall be able to Show Cansat Data on Computer Screen. Mission GS SW Low D,T GSE-04 GS SW Shall Provide Related Graphs on Computer Screen. Mission GS SW Low D GSE-05 GS Power Shall be Supported by Computer Connection. - GS HW Medium T GSE-06 GS Has NO Constraint on Mass or Power Budgets. - GS - - Elements: Antenna, Transceiver, Computer Interface, Software
15 System Architecture
16 Budgets and Schedule Payload-1 Payload-2 OBC COM EPS RCV STR Total GSE Mass (gr) Power (mw) Cost ( )
17 Thanks Questions?
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