Barrios Technologies project for Angelo State CS 4306 - Software Engineering
- Jeff Caldwell - jcaldwell2@angelo.edu
- Carlos Cardenas - ccardenas11@angelo.edu
- Josue Lozano - jlozano18@angelo.edu
- Jeremy Miles - jmiles10@angelo.edu
- Jonathan Morgan - jmorgan28@angelo.edu
- Ginger Kerrick, Chief Strategy Officer - ginger.kerrick@barrios.com
- Devin Vyain, Data Solutions Lab Supervisor - devin.a.vyain@nasa.gov
Mason Kindle, Graduate Assistant - mkindle@angelo.edu
Focus
Remember the following prompts for analysis, and center all of the effort around deriving insights into these prompts: Questions:
- What is the percent difference between historical consumable usage rate assumptions and actual calculated usage rates in mission time frames between resupply?
Answer: Overall historical usage on the space station for the time period covered by client data was 1.04% less than assumed usage rates.
- What resupply quantities are necessary, considering planned resupply vehicle traffic from the ISS Flight Plan, planned On-Orbit Crew counts, and historical usage rates to sustain minimum supply thresholds, plus a 10% safety factor, through the next two years?
Answer: Usage quantities can be found in the table below.
| event_date | vehicle_name | ACY Inserts | Air | Filter Inserts | KTO | Nitrogen | Oxygen | Pretreat Tanks | Urine Receptacle | US Food BOBs | Water |
|---|---|---|---|---|---|---|---|---|---|---|---|
| 2024-01-10 | Ax-3 | 63 | 282 lbs | 0 | 1 | 3 lbs | 52 lbs | 0 | 0 | 1 | 177 Liters |
| 2024-01-17 | DCC-1 | 172 | 484 lbs | 1 | 5 | 6 lbs | 177 lbs | 1 | 1 | 3 | 560 Liters |
| 2024-01-29 | NG-20 | 155 | 686 lbs | 1 | 4 | 8 lbs | 127 lbs | 0 | 1 | 4 | 431 Liters |
| 2024-02-15 | 87Progress | 27 | 121 lbs | 0 | 1 | 1 lbs | 23 lbs | 0 | 0 | 0 | 76 Liters |
| 2024-02-18 | Crew-8 | 136 | 605 lbs | 1 | 4 | 8 lbs | 112 lbs | 1 | 1 | 3 | 380 Liters |
| 2024-03-04 | SpX-30 | 346 | 1534 lbs | 2 | 9 | 18 lbs | 283 lbs | 1 | 2 | 7 | 962 Liters |
| 2024-04-11 | Boe-CFT | 182 | 807 lbs | 1 | 5 | 10 lbs | 150 lbs | 1 | 1 | 4 | 507 Liters |
| 2024-05-01 | HTV-X1 | 82 | 363 lbs | 0 | 2 | 4 lbs | 67 lbs | 0 | 0 | 2 | 228 Liters |
| 2024-05-10 | Ax-4 | 191 | 847 lbs | 1 | 6 | 10 lbs | 157 lbs | 1 | 1 | 4 | 532 Liters |
| 2024-05-31 | 88Progress | 273 | 1211 lbs | 2 | 7 | 15 lbs | 224 lbs | 1 | 2 | 5 | 760 Liters |
| 2024-06-30 | SpX-31 | 319 | 1412 lbs | 2 | 9 | 17 lbs | 261 lbs | 2 | 2 | 7 | 886 Liters |
| 2024-08-04 | USCV-9 | 136 | 605 lbs | 1 | 4 | 7 lbs | 112 lbs | 0 | 1 | 3 | 380 Liters |
| 2024-08-19 | 89Progress | 55 | 242 lbs | 0 | 1 | 3 lbs | 45 lbs | 1 | 0 | 1 | 152 Liters |
| 2024-08-25 | NG-21 | 191 | 848 lbs | 1 | 5 | 10 lbs | 157 lbs | 0 | 1 | 4 | 532 Liters |
| 2024-09-15 | DCC-2 | 611 | 1896 lbs | 4 | 17 | 23 lbs | 609 lbs | 3 | 4 | 13 | 1943 Liters |
| 2024-11-01 | PAM-5 | 291 | 1291 lbs | 1 | 8 | 16 lbs | 239 lbs | 1 | 1 | 6 | 811 Liters |
| 2024-12-03 | HTV-X2 | 36 | 162 lbs | 1 | 1 | 1 lbs | 30 lbs | 0 | 1 | 0 | 101 Liters |
| 2024-12-07 | 90Progress | 210 | 928 lbs | 1 | 6 | 12 lbs | 172 lbs | 1 | 1 | 5 | 583 Liters |
| 2024-12-30 | SPM | 9 | 40 lbs | 0 | 0 | 0 lbs | 7 lbs | 0 | 0 | 0 | 25 Liters |
| 2024-12-31 | SpX-32 | 291 | 1291 lbs | 2 | 8 | 16 lbs | 239 lbs | 2 | 2 | 6 | 811 Liters |
| 2025-02-01 | NG-22 | 45 | 202 lbs | 0 | 2 | 2 lbs | 37 lbs | 0 | 0 | 1 | 126 Liters |
| 2025-02-06 | USCV-10 | 164 | 726 lbs | 1 | 4 | 9 lbs | 135 lbs | 1 | 1 | 3 | 456 Liters |
| 2025-02-24 | 91Progress | 728 | 3228 lbs | 4 | 20 | 39 lbs | 597 lbs | 3 | 4 | 15 | 2027 Liters |
| 2025-05-15 | PAM-6 | 9 | 41 lbs | 0 | 0 | 0 lbs | 8 lbs | 0 | 0 | 1 | 25 Liters |
| 2025-05-16 | DCC-3 | 415 | 1170 lbs | 2 | 12 | 14 lbs | 428 lbs | 1 | 2 | 8 | 1354 Liters |
| 2025-06-14 | 92Progress | 437 | 1937 lbs | 3 | 12 | 23 lbs | 359 lbs | 2 | 3 | 9 | 1216 Liters |
| 2025-08-01 | NG-23 | 27 | 121 lbs | 0 | 0 | 2 lbs | 22 lbs | 0 | 0 | 1 | 76 Liters |
| 2025-08-04 | USCV-11 | 255 | 1130 lbs | 2 | 7 | 13 lbs | 209 lbs | 2 | 2 | 5 | 709 Liters |
| 2025-09-01 | 93Progress | 273 | 1210 lbs | 1 | 8 | 15 lbs | 224 lbs | 1 | 1 | 6 | 760 Liters |
| 2025-10-01 | CRS 2-24 | 282 | 1251 lbs | 2 | 8 | 15 lbs | 232 lbs | 1 | 2 | 6 | 785 Liters |
| 2025-11-01 | NG-24 | 228 | 1009 lbs | 1 | 6 | 12 lbs | 187 lbs | 1 | 1 | 4 | 634 Liters |
| 2025-11-26 | PAM-7 | 218 | 968 lbs | 1 | 6 | 12 lbs | 179 lbs | 1 | 1 | 5 | 607 Liters |
- What resupply quantities meet the requirements of question #2 while minimizing launch vehicle quantity? (e.g., launching 10,000 granola bars would ensure the minimum thresholds are not violated, but is not a realistic or optimal strategy for balancing launch mass requirements with supply requirements)
Answer: Resupply quantities listed in the table above meet the minimum launch vehicle quantity based on the schedule represented in the iss_flight_plan data.
- What month in the next two years of the Flight Plan timeline is most likely to incur a violation of minimum supply thresholds?
Answer: The time period most likely to incur a violation of minimum resupply thresholds is the period between launches in February, 2025 and May 2025.
- Which consumables item(s) are most likely to incur a violation of minimum supply thresholds in the next two years of the future Flight Plan timeline?
Answer: Water is the most likely consumable to incur a violation of minimum resupply thresholds.
Installation instructions are on the Installation Instructions page.
A user manual can be found on the User Manual page.
- Iteration 1: Requirements
- Iteration 2: Design
- Iteration 3: RAD and First Implementation
- Iteration 4: Design
- Iteration 5: Final Design Document
A slideshow presentation describing the project and its implementation can be viewed through the presentation pdf.