1. 2016 FMSR Team Name Full Mission Simulation Review (FMSR) University/Institution Team Members Date 1

2. 2016 FMSR User Notes You may reformat this to fit your design, but you must cover all the information requested on the following slides This template contains all of the information you are required to convey at this point in the project. If you have questions, please contact me directly: rocksatx@gmail.com or 303-492-4750 2

3. 2016 FMSR Purpose of FMSR: PLEASE READ: This review assumes - all individual subsystems have been tested - all hardware is in house - all mechanical items are machined - all individual subsystems have been tested together - a version of the flight software has been tested After successfully completing this review, your team will be ready for the Full Sequence Testing and Integration (FSTI) at Wallops 3

4. 2016 FMSR Presentation Outline 4 Section 1: Mission Concept and Interfaces Section 2: Design Overview Section 3: Individual Subsystem Test Status Section 4: Subsystem Integration and Test Status Section 5: Full Mission Simulation Results Section 6: Project Schedule Section 7: June Operations Section 8: Conclusion

5. 2016 FMSR 1.0 Mission Concept and Interfaces Name of Presenter 5

6. 2016 FMSR Mission Overview 6 One slide only Present a concise Mission Statement What do you expect to discover or prove? Who will this benefit/what will your data be used for? Make your case as to why this mission should fly on a rocket

7. 2016 FMSR Success Criteria: 7 Minimum Success Criteria: –What is the least amount of data you can collect that will still constitute a success? Comprehensive Success Criteria: –What is the ideal amount of data to have full or comprehensive mission success?

8. 2016 FMSR -Please confirm your mounting location Payload Location

9. 2016 FMSR Activation Sequence: 9 EventTime OnDwellEvent Description GSE 1T-180 sec540 sec Minutes before launch. Start on the computer for the experiments. GSE 2T-180 sec540 sec Minutes before launch. Start on the computer for the experiments. TE-1T+000 sec360 secLaunch TE-2T+000 sec360 secBring more power to RGA's. TE-3T+000 sec360 secBring more power to RGA's. TE-RT+000 sec360 secBring more power to RGA's. Please confirm your team’s Timer Events Matrix Update your team’s slide and delete the others If a sharing with another payload, list events used by other payload

10. 2016 FMSR Pin Assignments: Power 10 Power Connector--Customer Side PinFunction 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 Fill-in the function side for your payload If not using, put N/A If sharing connector indicate other team’s name in function side Check for consistency with User’s Guide

11. 2016 FMSR Pin Assignments: Telemetry 11 Fill-in the function side for your payload If not using, put N/A If sharing connector indicate other team’s name in function side Check for consistency with User’s Guide Telemetry Connector--Customer Side PinFunctionPinFunction 1 20 2 21 3 22 4 23 5 24 6 25 7 26 8 27 9 28 10 29 11 30 12 31 13 32 14 33 15 34 16 35 17 36 18 37 19

12. 2016 FMSR Updated Power Budget 12 USE Power Budget xls file Include a screenshot in your presentation and the actual excel file with your CDR package I am most interested in total amp-hours since each payload space is allowed 1 Ah. Voltages and currents should also be included. ExampleSat Power Budget SubsystemVoltage (V)Current (A)Time On (min)Amp-Hours STR0000.000 DEP120.420.013 EPS280.3200.100 PM280.980.120 … … … … Total (A*hr):0.233 Over/Under0.77

13. 2016 FMSR Detailed Weight Budget 13 ExampleSat Mass Budget SubsystemTotal Mass (lbf) STR2 DEP8 EPS12 PM9 … … … … Total31 Over/Under(1.00) Present your subsystem weight and total weight similar to what is given at right Full payload spaces must = 30+/-1.0 lbs Shared payload spaces must = 15+/-0.5 lbs –Weight of payload deck is 3.425 lbs Include ballast and harnessing so total meets requirement

14. 2016 FMSR User Guide Compliance 14 RequirementStatus/Reason (if needed) Center of gravity in 1" plane of plate? 1.2" currently Weight 30.0+/- 1.0 (15.0 +/- 0.5) lbs? 31.5 lbs (working on reducing) Max Height < 10.75” (5.13”) 10.9 inches (waiver requested) Bottom of deck has flush mount hardware? YES, see picture on slide XX Within Keep-Out Zone YES, see picture on slide XY Using < 10 A/D Lines Using on 8 lines Using/Understand Parallel Line N/A Using/Understand Asynchronous Line YES, at 19200 Baud Using X GSE Line(s) YES, GSE 1 and GSE 2 Using X Non-Redundant PWR Lines (TE-1, TE-2, TE-3) YES, TE-1 and TE-2 Using X Redundant Power Lines (TE-R) YES, TE-R Using < 1 Ah 1.1 (working on reducing) Using <= 28 V 200 V (Will conformal coat) Using RF (If yes, list frequency and TX Power) YES, 134.34 MHz @ 1 watt TX power Using deployable? YES, but speed is under 1 inch per second Whole team consists of US Persons YES Using ITAR and/or Export Controlled hardware NO

15. 2016 FMSR 2.0 Design Overview Name of Presenter 15

16. 2016 FMSR System Changes Since ISTR 16 Please update me on your actions assigned during ISTR (list them) What major changes have you made since ISTR? –Why were these changes made? Do these change any of your mission objectives/requirements?

17. 2016 FMSR Design Overview: 17 Present top, side, and multiple iso views on individual slides If you have deployments or extensions, include side views of extended and retracted modes A high level of detail is expected as these images will be used for your pre-launch inspection by Wallops personnel in June/August If you have deployments, indicate how long items will be deployed

18. 2016 FMSR Hazardous Mechanical Items: 18 Identify all materials that may be considered hazardous Identify all mechanical operations that may be considered hazardous (stored energy, deployments, etc) If you have deployments, include length of travel when deployed and time it takes (i.e. 3 inches in 6 seconds) Identify all mechanical components that may hazardous or interfere with other payloads or rocket systems (magnets, transmitters, items that change your CG or MOI during the flight)

19. 2016 FMSR Hazardous Electrical Items: 19 Identify any high voltage items/components Identify any operational hazards with your electrical design

20. 2016 FMSR Special Requests Please describe any special requests of the rocket and/or Wallops that are required for minimum and/or comprehensive mission success Examples include but are not limited to: –Extra volume –Extra weight –High voltage –Extra telemetry –Faster sampling –Special environmental considerations 20

21. 2016 FMSR Update on Partnerships Please update details with any partnerships with sponsors and/or collaborators Looking for details on the how partners will interact with students to bring the payload to launch readiness What will be the role(s) of the partners? What will they be providing to the mission and students involved? Partnerships must have significant student involvement and cannot be simply flying hardware on a student launch opportunity. 21

22. 2016 FMSR 3.0 Subsystem Testing Status Name of Presenter 22

23. 2016 FMSR Functional Block Diagram: FBD should show –HOW subsystems interact with each other –HOW data moves (recorded, stored, telemetry) –HOW power and data flow through subsystems (include voltage levels and data line types) –Show mechanical and electrical inhibits –Show Wallops interface (power/telemetry) and include GSE and TE lines –All individual subsystems should be fully tested by this review 23

24. 2016 FMSR Subsystem Testing Status: 24 List all the subsystems in your payload with % complete of testing at the subsystem level Must match subsystems called out in your Functional Block Diagram above Don’t forget to discuss your software If a subsystem is not 100% tested, indicated what items still need to be tested Duplicate following slide for each subsystem

25. 2016 FMSR Subsystem Testing Status: 25 Subsystem A X, Y, and Z have been tested with great success Q, W, E, R, T, and Y where tested but failed due to the invasion of fire ants A, B, and C have not been tested but will be by April 30, 2013 75% Include pictures and/or screen shots of data or test USE this slide for each subsystem

26. 2016 FMSR 4.0 Integrated Subsystem Testing Status Name of Presenter 26

27. 2016 FMSR Integrated Subsystem Testing Status: 27 Create a list with the order that subsystems were integrated and tested Include mechanical integration on the list Can be parallel activities List the status of each of these steps using copies of the following slide State the purpose of integration/test State the results of these tests If no results, describe how and when the test will be completed

28. 2016 FMSR 28 1.0 Subsystem A and Subsystem B This will verify that the flux capacitor and the plutonium reactor work properly Test was completed on April 13 th with great success Additional tests will be conducted next week 75% Include pictures and/or screen shots of data or test Integrated Subsystem Testing Status: USE this slide for each integrated subsystem

29. 2016 FMSR 5.0 Full Mission Simulation Results Name of Presenter 29

30. 2016 FMSR Full Mission Simulation Results: 30 Discuss the results so far on any Full Mission Simulations that you have completed Include pictures of hardware Include pictures of set up Include pictures/plots of data Include picture of hardware connected to Wallops power and telemetry connectors Include pictures/videos of deployments Include pictures/videos of experiments in action

31. 2016 FMSR Full Mission Simulation Results: 31 Discuss the overall results of the simulation Discuss plans for follow on simulations Discuss aspects of your mission that simulation did not test Discuss anything that was discovered during the simulation

32. 2016 FMSR 6.0 Project Schedule Name of Presenter 32

33. 2016 FMSR Schedule 33 Present a detailed schedule for April, May, and June

34. 2016 FMSR 7.0 June Operations Name of Presenter 34

35. 2016 FMSR June Operations: 35 Detail the steps you will follow to operate your payload with or during the: RS-X GSE Sequence testing with Wallops GSE Vibration testing Post-vibe sequence testing with Wallops GSE (GSE = Ground Support Equipment)

36. 2016 FMSR June Operations: 36 Describe all aspects of your payload that will not be present or available for testing in June

37. 2016 FMSR June Operations: 37 Describe what features of your payload cannot and/or will not be tested on the ground and the reasons why

38. 2016 FMSR June Operations: 38 Include a screenshot of your team’s checklist that will be used at Wallops to remove and/or install mechanical and/or electrical inhibits for testing in June List the steps on your checklist here

39. 2016 FMSR 8.0 Conclusions Name of Presenter 39

40. 2016 FMSR FMSR To FSTI: 40 Level of confidence that your team will be ready for Full Sequence Testing and Integration What are the major hurdles going to be?

41. 2016 FMSR Worries and Concerns 41 List your biggest worries and concerns related to you project at this moment Discuss your plans for mitigating these items