Frequently Asked Questions
Answers to questions we often get about the BIRDS bus and its integration into custom projects
1. Rationale for Vacuum Leak Test Before Vibration Test
testing
-
Reasoning:
- The primary reason for performing the vacuum leak test before the vibration test was scheduling adjustments.
- Performing the tests in reverse order (vibration test first, then vacuum test) is technically feasible and does not pose any issues.
-
Procedure Alignment:
- It is recommended to follow the established procedures from previous BIRDS projects unless there is a strong justification for deviation. Consistency ensures comparability and adherence to best practices.
2. Can we borrow a weight measurement device at Kyushu Institute of Technology (Kyutech)? (The mass should be measured to three decimal places.)
structure
Yes, it can be lent out.
3. It seems that there is only one uplink detection code (ASCII code) in BIRDS. Is it possible to set two on the COMM board? To ensure uplink security, can multiple ASCII codes be configured?
communications
Yes
4. I am considering mounting a patch antenna and a magnetic torquer on a newly developed satellite. Could you provide information about the magnetic torquer used in Kyushu Institute of Technology’s BIRDS satellites (such as the manufacturer and product name)?
adcs
The details of the magnetic torquer coil are mentioned in the master’s thesis of Hisatsugi, who designed the ADCS for BIRDS-4. The design is described in Chapter 11.6 (page 90) and summarized in Table 11.19 (page 95). BIRDS-4 was launched with these magnetic torquers, but they were not activated in orbit due to other mission priorities.
5. How were the orbital parameters of the BIRDS-III satellites determined after deployment?
mission
The orbital parameters were initially provided by the launch provider. These were then refined using ground station data and TLE data from organizations like NORAD.
6. Is it possible to know the current location of the BIRDS-III satellite using TLE data?
mission
Yes, you can track the satellite using TLE (Two-Line Element) data. Tools like GPredict and Orbitron allow you to input TLE data and calculate satellite position.
7. How were the deorbiting strategies implemented for BIRDS satellites?
mission
The satellites relied on natural orbital decay due to atmospheric drag. They were designed with low orbital altitudes to ensure re-entry and burn-up within a few years.
8. What were the specific conditions during the thermal-vacuum test for BIRDS-III?
environmental-testing
The test conditions vary by launch provider. In BIRDS-III, they were based on ISRO’s requirements. Coordination was done with the provider accordingly.
9. Apart from vibration and thermal vacuum tests, what other tests are conducted?
environmental-testing
Additional tests depend on satellite design. Refer to open-source documentation from Kyushu Institute of Technology.
10. What kind of testing was done to ensure that the BIRDS satellites could withstand vibration during launch?
environmental-testing
Sine, random, and shock vibration tests were conducted per launch provider specifications to verify satellite durability.
11. How long is one cycle of the thermal cycle test? What is the interval between cycles? Were 100 cycles performed?
environmental-testing
About 100 cycles are typically performed to ensure robustness.
12. Do you use the -15°C to -20°C to 60°C thermal cycle test range for non-outer panel tests?
environmental-testing
In some cases, the range is wider (e.g., -80°C to 60°C) as shown in the solar cell adhesive thesis.
13. Please tell me the name of the test equipment used for the thermal cycle tests in the solar cell thesis.
environmental-testing
-
LaSEINE’s constant temperature chambers:
- 83_小型恒温槽機取説20200521_short version.pdf
- 83_大型恒温槽_参考資料_2018.pdf
14. I would like to reference a paper on the relationship between strain measurement and thermal cycles for implementing the thermal cycle test.
environmental-testing
Reference: 84_20220307_熱サイクル試験.pdf
15. For the camera system used in BIRDS-III, was there a specific manufacturer or a custom-built component?
payload
The camera was a ready-made module. Specifications and performance details are in attached documents.
16. Were there any challenges integrating the payloads into BIRDS satellites?
payload
Challenges included managing limited space, thermal management, and electromagnetic interference.
17. How do you think about the phenomenon of static electricity in wood in space?
payload
Dry wood has high resistivity, slightly lower than Kapton. Electrostatic precautions similar to plastic apply.
18. If there are detailed materials on geomagnetic sensor calibration, could you share them?
adcs
Yes. Refer to the master’s thesis of the ADCS designer for BIRDS-4.
19. I would like to receive the ground and flight data for the geomagnetic sensors from BIRDS-3 and BIRDS-4.
adcs
Materials include:
- 91_magnetometer.c
- 91_GLEX-2021,7,1,14,x62750[16].pdf
20. I am controlling the COM board via UART from the PC, but the ground station cannot receive data. Could you provide the packet format and content?
communications
Check the COM PIC program. Using the OBC board is recommended over the PC.
21. Who should I contact at JAXA regarding spring plungers?
structure
Contact the supplier directly.
22. Are jigs used for precise assembly in BIRDS?
structure
No extra jigs are used. Spacing is confirmed using calipers.
23. How is the battery box secured?
structure
It is fixed using four shafts, like other boards.
24. How was radiation shielding designed in BIRDS?
structure
Structural materials were leveraged. Critical components were selected for radiation tolerance.
25. What precautions were taken for thermal stability in BIRDS-III?
structure
Passive control methods, coatings, and TV tests were used.
26. What simulation tools were used to analyze structural integrity?
structure
ANSYS and SolidWorks Simulation were used for various simulations.
27. What are the allowable tolerance levels for structural components of BIRDS-IV?
structure
Depends on the deployment mechanism and launch specs. See design docs.
28. What operating temperature range is assumed for mission board components?
hardware
No fixed range, but industrial-grade components are preferred.
29. What are the weights of the boards used in BIRDS?
structure
- FAB: 36 g
- Battery Box: 267 g
- RF Shield: 12 g
- OBC/EPS: 33 g
- COMM: 102 g
- RAB: 63 g
- BPB: 46 g
- Antenna board: 60 g
30. Are the spacers used in BIRDS commercially available or custom? Are there differences between BIRDS-4 and BIRDS-5 boards?
structure
MISUMI spacers are used. No changes between BIRDS-4 and BIRDS-5 for FAB and OBC/EPS dimensions.
31. How was the ground station software for BIRDS-IV developed? Was open-source software used?
ground station
Yes, built on open-source frameworks with added custom functions.
32. Were any COTS components used in BIRDS?
hardware
Yes, including microcontrollers and camera modules.
33. What were the main lessons learned from BIRDS-III that influenced BIRDS-IV?
lessons learned
- Improved subsystem integration and testing
- Better documentation
- Optimized payload management
- Stronger collaboration
34. Who does Kyutech outsource new mission board designs to?
procurement
Designs are created at Kyutech, fabrication by P-ban.
35. Who is the P-ban staff in charge of BIRDS?
procurement
There is no dedicated staff person.
36. Which company does P-ban.com buy PCBs from?
procurement
P-ban.com manufactures PCBs and assembles them from Eagle files.
37. How can I output Gerber data for more than 6 layers in Eagle?
procurement
Use the attached Gerber output library: 85_BIRDS_6layer (1).cam
38. Since the effective control space of the Helmholtz coil is ±70mm, is it correct to assume that a 1U-sized satellite with a ±100mm range will fit within this control space?
environmental-testing
The effective control space of the Helmholtz coil is ±70mm, so a magnetometer mounted inside a 1U CubeSat should be able to be tested without issues. According to the person in charge, they have previously conducted measurements on a 2U satellite.
Whether the magnetic sensor is within the effective control space depends on the sensor’s mounting position, so the mounting location of the sensor needs to be confirmed.
39. Is the type of converter for the chamber SMA for both the inner and outer parts, or is it N-type?
hardware
The connection is SMA.
40. I would like to know the minimum and maximum temperatures of the external panel measured in BIRDS.
environmental-testing
I would appreciate it if you could share reference materials regarding the TVT (Thermal Vacuum Test) temperature settings for BIRDS.
41.
① If there is a program that automatically saves data obtained from ground tests to Excel or similar formats, I would appreciate it if you could share it.
② Is the data obtained during satellite operations through downlink saved by methods other than pressing the Save button on the ground station app?
ground-station
① No.
② Currently, the software used at Kyushu Institute of Technology has an automatic save function.
42. A letter has arrived regarding the ITU procedure. Could you please guide me on how to proceed?
licensing
I will check with the Ministry of Internal Affairs and Communications regarding the process.
43. Has a similar situation occurred in BIRDS satellites where the voltage was around 3.2V right after antenna deployment?
integration-test
Yes, but the sensor condition depends on battery charge.
44. What kind of cable was used in BIRDS to connect the ground station and the chamber?
hardware
We used SMA cables.
45. Was a dedicated command used for downlinking HK data during BIRDS satellite operation?
integration-test
No, the downlink was done by specifying the address area.
46. Only ResetPIC did not respond when all boards except the battery were operated. What should be done?
integration-test
We will test with the open-source program.
47. Has a program for data deletion been created in BIRDS before loading the FM program or testing?
obc
Yes, check analyze_command.c of Main PIC.
48. Are CW1 and CW2 transmitted alternately, and is CW3 needed for sending mission data?
obc
Yes, and a custom program is necessary for CW3.
49. How is the body diode issue handled in SepSW1 (P-channel MOSFET)?
safety-review
Reverse current occurs; a DC-DC converter prevents it.
50. What paint is used on the chamber shroud, and what is its structure?
environmental-testing
The black paint is a spray with emissivity of 0.94; the chamber is copper, covered with MLI.
51. What measurements are required for satellite station completion inspection, and are any materials available?
licensing
Confirm with the bureau or measurement service provider.
52. What evaluation criteria were used for E2E testing?
integration-test
Evaluation included antenna deployment, OBC, CW, downlink, etc.
53. Has damage to the FAB board DEP SW4 circuit occurred before in BIRDS projects?
integration-test
No similar problems have been reported.
54. What type of terminal is attached to the small chamber?
environmental-testing
See: 118_Small Chamber Manual_Ver2019.pdf
55. What items were included in the “Physical Characteristics List” for reentry risk evaluation?
space-activity
Used for Space Activity Law compliance.
56. What is the melting point of CMX100 cover glass used in the solar panels?
space-activity
Softening point ~850–900°C; melting point ~1650°C.
57. Has the battery temperature ever exceeded the allowable range during BIRDS thermal vacuum testing?
environmental-testing
No, it ranged from -2 to 55°C in BIRDS-5.
58. What factors were considered when determining the BIRDS-5 thermal vacuum test profile?
safety-review
59. Why was the number of antenna deployment attempts in BIRDS-5 set to four, and could communication failure be related?
integration-test
The procedure was inherited; the cause of failure was inconclusive.
60. What is the minimum battery voltage required for steady operation during ground tests?
integration-test
Downlink succeeded at 3.6V. Analyze E2E test data.
61. What is meant by “criteria used to power on the system” during FM testing?
integration-test
Clarification requested.
62. Was the shutdown due to the 24-hour Reset PIC trigger or packet communication failure?
integration-test
Possibly Reset PIC issue; program investigation recommended.
63. Is the current limit of the FAB’s DC-DC converter the reason for downlink failure when using J5 and RBF2?
hardware
Yes.
64. Why is RBF2 inserted when supplying power from J5, and is it removable in orbit?
integration-test
birds-3
It simulates solar cell generation. Refer to the BIRDS textbook.
65. Please share information regarding SAR 6.1.
safety-review
Refer to: https://birds-project.com/opensource/
66. Please share information regarding SAR 3.2.4.
safety-review
Refer to: https://birds-project.com/opensource/
67. How will the battery voltage and capacity be measured after assembly?
eps
The voltage will be measured from the access port. Based on the voltage data, the capacity will be calculated using the results from the battery screening test.
68. What is the effect of ΔV after CubeSat deployment from the pod, and can the release orbit be specified?
structure
ΔV is typically between 1.1–1.7 m/sec. The release altitude during the ISS release (380–420 km) affects this. Users cannot specify the orbit.
69. What is the expected daily usable mission data downlink, considering HK and overhead?
communications
Approximately 20 kB per operation. With about 2 usable passes per day, around 40 kB can be downlinked daily.
70. What are the GPS specifications, including ICD information (mass, power, data rate)?
mission
Fireant GPS is used. SkyTraq S1722F8-GL IC. Mass: 45g; Size: 45mm × 35mm; Power: <0.3W; Format: NMEA (ASCII), 900 chars/sec, 1Hz output.
71. What are the changes from BIRDS-3 to BIRDS-5?
obc
References provided: FAB and OBC revisions.
72. What is the part number of the CPLD on the BPB?
obc
Reference files include BOM and Testbed.
73. What is the frequency coordination guide and process?
licensing
Domestic coordination begins with API submission. Recommended to contact regional bureaus in advance. Telecom Guide PDF
74. What are the deadlines for Phase 0, 1, 2, and 3 of development and safety review?
safety review
Development and review timelines vary, but total review time can be 1.5 to 2 months. Example timelines for BIRDS-2 to BIRDS-4 are detailed.
75. Who provides reference documents like CR-99117 and CR-99218 for MIUL writing?
safety review
They are only accessible to JAXA contractors under NDA.
76. Is it acceptable to use MIUL formats like MSFC-HDBK-527F or MAPTIS2?
safety review
CubeSats use MIUL as a summary, not material-specific. JAXA/contractor determines use.
77. What materials are listed in MIUL, including internal parts like semiconductors and camera?
safety review
MIUL lists the satellite as one entity; individual components are not detailed.
78. Do we need material certificates for all materials used?
safety review
Primarily for outer FR4 substrates and structural fasteners. Required if classified as Fracture Critical Parts. Vibration testing may substitute if unavailable.
79. What is the hazard report (SHR/UHR) format for Phase 1 09-12?
safety review
Not public. Contractors can provide drafts. JAXA/NASA define the structure. Diagrams and tables recommended.
80. Please indicate the areas to be potted on the FAB board.
safety review
The areas to be potted are shown in the submitted documents. Please verify the submitted materials.
81. Please explain the working environment and content during the final charging.
safety review
It will be conducted as described in the safety review document UHR.
82. I would like to refer to the Inhibit Function Test Report for BIRDS-5.
safety review
Please verify what tests (or verifications) are necessary based on the safety review materials submitted so far.
83. How did Kyushu Institute of Technology classify and manage this fastener?
structure
84. Please share the Antenna Storage Procedure Manual or equivalent.
safety review
Check the AP for equivalent documentation.
85.I would like to know about the analysis of the temperature rise of the battery heater.
eps
No analysis done; safety verified by testing the downstream FET.
86. Was the reverse current prevention function of the DCDC converter tested?
eps
Yes. Reverse voltage applied; capacitor voltage measured pre/post DCDC.
87. How to verify DCDC reverse voltage characteristic post-assembly?
eps
Check SRC_V after RBF2 removal in a dark room; no solar effect expected.
88. Is it possible to verify SepSW1’s health and reverse current prevention?
eps
Use power supply bias and monitor SRC_V during SepSW1 ON-OFF.
89. TNC is in TERMINAL mode, not KISS.
communications
90. USB radio, antenna, and cable vendor info request.
communications
See reference: 147_Student Experiment Parts List.xlsx
91. Share power budget table for BIRDS-4.
eps
Reference: 151_Power_consumption_generation_BIRDS4.pdf
92. RTV supplier and usage guidance.
eps
Supplier: Hayakawa Shouji Co. Ltd. Mix S-691A (0.9kg) and S-691B (0.1kg) in 9:1 ratio.
93. Is a 90W, 5A 18V programmable power supply sufficient for screening?
eps
Yes. 1C = 3.5A. Setup acceptable.
94. Evaluation request: Tokyo Keiki shield box vs. my1515.
communications
Keiki box more suitable for UHF than my1515. Specs confirm 60dB shielding; used in past projects.
95. Share Space Activity Law Handbook.
safety review
96. Request for data/papers on radiation for thermal design (NASTRAN).
structure
STM and thermal vacuum testing recommended for accurate modeling.
97. Regarding hazards, section 4.2.2.1 of JX-ESPC-101132-D lists only four standard hazards, but this document lists fourteen. Is this because the hazards required for small satellites and other satellites are different?
safety review
In section 4.2.2.1 of JX-ESPC-101132-D, standard hazards are listed as “examples of responses” and include 14 items.
98. Is it better to clearly document the hazard report using FTA?
safety review
Refer to the SAR available in BIRDS Open Source.
99. A glass bandpass filter and camera are used. Does this correspond to the standard hazard “Prevention of glass and other fragments”? Also, it appears that BIRDS-4 does not have a cover on the lens, but how was this approved?
safety review
When using glass, there are three possible ways to address this:
- The glass is encapsulated
- The design ensures no load is applied
- Other methods to control it
In the case of BIRDS, verification documents demonstrated safety through UHR and vibration testing.
100. I would like to share the SAR document.
safety review
Refer to the SAR available in BIRDS Open Source. Document according to the format provided by the contractor.
101. How were the permanent magnets and hysteresis dampers procured?
ADCS
102. Has BIRDS used thermal control elements in the past (e.g., heaters, Peltier blockers, etc.)?
thermal
Heaters were used until BIRDS-4, but from BIRDS-5 onward, they were not included. Model used: KHLVA-102/10 Heater Model Link
103. What materials are used in the frame of BIRDS-4 and for what purpose?
Structure
PEEK was used for insulation where the frame acted as the antenna. BIRDS-5 reverted to full aluminum.
104. Should the documents submitted to the Ministry of Internal Affairs and Communications (MIC) be prepared before the JARL documents?
Licensing
JARL documents can be submitted first. A ground station call sign can be secured early by explanation to the General Communications Bureau.
105. What parameters need to be entered for the following?
- EIRP of the satellite transmitter
- Adjustment range of UHF communication equipment
- Noise temperature
- Reference bandwidth
- Modulation loss
- Noise bandwidth
EIRP = Ptx [dBm] - L [dB] + G [dBi]
106. I need the antenna pattern diagram from Kyushu Institute of Technology.
Communications
See attached document: 175_BIRDS_GS_Antenna_M2.pdf
107. What tests are required for battery screening and how were EM tests done at Kyutech?
Screening follows JSC-20793; FM cells must be verified. EM tests are optional unless used for FM verification.
108. How is the inspection carried out after the vibration test when FM cannot be disassembled?
Structure
Torque marks are checked via holes in outer panels or outer panels are removed and reassembled per manual.
109. I am searching for bypass diodes for solar cells. Is MBR1020LL acceptable despite different temperature range?
EPS
Yes, a −55°C range is acceptable.
110. Can I get downlink measurement results from Kyutech since the spectrum analyzer is broken?
Communications
Yes, see: 179_BIRDS-4 Downlink Measurement Data.pdf
111. STK shows a different beta angle than the document for June 1, 2021. Can you confirm this discrepancy?
EPS
Also, power generation values under same beta angle differ. Reference: 180_Power-Budget-Analysis-for-1U-satellite_Final.pdf
112. What was discovered about FET-based over-discharge control and what changes may be required?
Safety Review
Three inhibits are required. Parasitic diode behavior in Pch MOSFETs complicates isolation, needing redesign.
113. Is the leakage current from Dep SW2 sufficiently small to ignore?
Safety Review
Yes, current is minimal and within safe limits. Reference: 182_DepSW_電流.png
114. What is the gender of the Dsub25 connector inside the Peltier chamber?
Environmental Test
Interior connector is female, exterior is male.
115. We plan to use an external vibration machine. Are there spec issues?
Environmental Test
Specs will be cross-referenced with JAXA documentation.
116. What is the material of the black paper-like substance used in the battery screening test?
EPS
Reference: 185_Battery Screening .jpg
117. How does Kyutech measure charge and discharge characteristics after FM assembly?
Safety Review
Only OCV (Open Circuit Voltage) is measured after FM assembly.
118. What is the concern with antenna material combinations, and how was it addressed in BIRDS?
Safety Review
Tin-plated Cu wire caused corrosion with SK85 steel. BIRDS switched to plain Cu wire and coordinated with contractor.
119. Can you share the BIRDS-5 packing and delivery procedure manual?
Safety Review
Refer to the BIRDS-5 documentation.
120. Kazakhstan and Thailand raised interference concerns with YOMOGI satellite. What was the response?
Licensing
Awaiting follow-up for frequency application and countermeasures.
121. I have heard that the integrated development environment for handling ground station programs is Visual Studio. Are you using the free version, Visual Studio Community, or the paid version, Visual Studio Professional?
Ground Station
It seems that development can be done without any issues using Visual Studio Community.
122. When checking commands, I heard that you are testing by placing the antenna inside an aluminum box. Could you share which box you purchased, or provide a photo if available?
integration-test
123. The BIRDS platform states that “ResetPIC and COMPIC communicate via UART.” In fact, the circuit diagram for BIRDS5 also shows a UART connection between the two PICs. However, the UART for COMPIC is not defined in ResetPIC, and the code does not include any communication between ResetPIC and COMPIC via UART. Could you please explain this difference?
obc
Regarding the UART between COM PIC and Reset PIC: First, the UART communication between COM PIC and Reset PIC is just included as a feature. It is not used in the current design. Therefore, while it is marked as UART in the circuit diagram, it is not included in the program.
Regarding the definition of RB6 and RB7 as UART lines in Reset PIC: The purpose of defining RB6 and RB7 as UART lines is likely to enable direct debugging and program verification during the construction of the Reset PIC program. When performing debugging through the access ports on the FAB, it is necessary to go through the Main PIC. However, in case of debugging failure, it is unclear whether the issue is with the Main PIC or with the Reset PIC not functioning as expected. Therefore, it is believed that the goal was to allow data to be sent directly from the Reset PIC to the PC.
124. Regarding the battery heater section: Is my understanding correct that RD0 = 1 turns the battery heater ON and RD0 = 0 turns it OFF?
Does the voltage output from the temperature sensor inside the battery box decrease as the temperature increases?
obc
125. As seen in the attached schematic, the DEPSW4 signal is interrupted at J15 within the FAB, and it seems that the signal does not reach Q9 and Q10. Is this intentional, or did Kyushu Institute of Technology later solder connections to ensure continuity?
obc
This is part of the specification. A jumper pin has been installed. Reference: 87_BIRDS BUS Board_Jumper Pin.png
126. How were software updates and patches handled for BIRDS satellites after launch?
software
Software updates were not possible after launch due to hardware constraints. Therefore, robust testing of the satellite software was performed prior to launch to ensure reliability and minimize potential issues in orbit.
127. There is a suggestion that it might be good to set multiple uplink detection codes. If it is possible to set multiple uplink detection codes, I would like to know how to control and differentiate between them. If you have any information regarding this, I would appreciate it.
com
It is possible, but I believe the current setup is sufficient.
128. Regarding the wire connecting the antenna element to the SMA connector on the board’s back, what material was used? How was the wire connected to the element? Was the element’s surface processed (e.g., sanding)?
com
The wiring was done using the leads of DIP resistors. The element surface was sanded with sandpaper. For connections, the resistor lead was routed from the board and temporarily fixed to a bolt, leaving a 2mm gap. The lead was wrapped 1.5 times clockwise around the bolt, which was then tightened.
129. For the PhotoMOS used in the nichrome wire heating circuit, what was the part number and how was it mounted?
com
The part number is AQZ102. Although it is currently out of stock, this DIP component was modified by bending its leads for SMD mounting before assembly. Digikey Product Page for AQZ102
130. Are there any recommended processing companies for the antenna fixture?
com
These were likely created in the Kyushu University workshop. Since it is not particularly difficult to process, you can also commission companies that manufacture metal structures.
131. For the antenna wire, should hole drilling be requested from Osaka Heat Treatment Co., Ltd., or should it be commissioned to another company?
com
For BIRDS-4, only materials were purchased, and hole drilling was done in the laboratory. However, this process is labor-intensive and not recommended (wires often break). It’s better to contact a company specializing in metal structure manufacturing.
132. Is outsourcing necessary for processing the nichrome wire into a coil, or can it be done in the university?
com
Nichrome wire coil processing does not require outsourcing; it can be done in the laboratory.
133. What types of antennas were used for communication in the BIRDS project, and what were their specifications?
com
The BIRDS satellites typically used monopole or dipole antennas for communication in the UHF and VHF frequency bands. Detailed specifications are available in the communications subsystem design document.
134. Adnics said the BIRDS project uses 180 mm cables, but it seems there is excess length. How was the excess cable stored?
com
The excess coaxial cable was stored between the antenna board and the RAB.
135. How was the SMA cable routed from the COMM board to the antenna board? Was the cable fixed along the way?
com
The SMA cable is soldered to the Addnics COMM board (UHF TRX). Normally, the cable is routed on the top side (+Z direction) of the board to the antenna board. The cable was taped to suppress vibrations. During final FM assembly, the SMA connector was torqued to 56 N·cm, and Araldite was applied to prevent loosening.
136. The element material is slippery and difficult to drill. How was positioning handled?
com
Positioning was done by scribing. Wood was placed underneath the antenna during drilling. A standard drill press was used with a sharp, rust-free drill bit. Fixtures and templates were created for precision.
137. What precautions are taken regarding uplink encryption and disclosure of uplink frequency in the BIRDS satellites?
com
Uplink frequencies are not disclosed externally and are displayed as placeholders like “430.XXX [MHz]” in internal docs. Although encryption of commands is technically used, fully encrypted communication is not permitted in amateur radio bands. Pseudo-encryption is used and accepted during frequency coordination.
138. I would like to request the Excel file or guide related to the BIRDS link budget calculation if available.
com
The link budget Excel for BIRDS-5 is available. Input the frequency in row 3 and device sensitivity data in row 31. Reference: 119_120_121_BIRDS-5 LinkMargin.xlsx
139. Is it acceptable to modify the BIRDS link budget Excel file to include the ground station’s 31 dB preamp?
com
Yes. The preamp amplifies both signal and noise, so link margin improvement is about 3 dB. Adjust cable loss and noise temp in rows 29 and 30 respectively. Reference: 119_120_121_BIRDS-5 LinkMargin.xlsx
140. How should I calculate the noise temperature from the preamp’s noise figure (NF), and what value should be input in the Excel file?
com
For NF of 0.2 dB, the noise temp is ~14 K. Use 290K as room temperature. The Excel sheet expects Kelvin in row 30. Refer to:
141. In designing the mission circuit of the Birds system, what are the conditions for the supplied voltages and signal inputs and outputs?
eps
Depending on the design of the BUS system, the BIRDS satellite can use 3.3 V, 5 V and Battery line for the mission system, while the Battery line voltage will vary between 3.8 V and 4.2 V, depending on the satellite. The maximum current value that can be used by the mission system depends on the design of the satellite.
142. What is the degree of fluctuation in the 5V power bus?
eps
There is no specific information available about fluctuations in the 5V power bus.
143. Does the mission board need an A/D converter for digital output? Is an analogue output of the measurement results sufficient?
eps
In the case of BIRDS, two methods are used: digital data is sent from the Mission system via UART or to the Flash Memory on the OBC board using SPI.
144. How is the discharge test conducted, and are there other ground tests necessary for the EPS system?
eps
The battery is the most critical component for satellite safety. Testing the battery and verifying the operation of the deployment switch after satellite assembly are key ground tests for the EPS system. However, safety reviews may result in changes, so specific test items need to be confirmed in consultation with JAXA. Attached are materials summarizing the types and flow of battery tests conducted at Kyushu University.
145. How is the electronic load used in the cell screening test? Should CV mode be used to prevent overcharging above 1.6V? Why does the voltage in the attached graph change above 1.6V when using CV mode?
eps
Battery screening requires an electronic load, multi-range power supply, data acquisition system, LabVIEW-based test control software, and test batteries. The electronic load is used in CC mode during battery discharge and is controlled by LabVIEW software. The program also controls the DC power supply. For NiMH batteries, the -dv/dt method is used to safely end charging, taking 10 minutes to detect full charge and stop. Screening tests at room temperature in CC mode are recommended. The maximum voltage can be controlled at 1.6V. Conduct charge/discharge tests at a rate of 1C.
146. Was the digital conversion module of the DAQ used in the LabVIEW diagram for the battery screening test of BIRDS-III?
eps
Instead of using a digital conversion module, the electronic load device was controlled via VISA communication from LabVIEW. This method was used in the past at Kyutech using Kikusui’s electronic load device.
147. What types of batteries were used in the BIRDS-III satellite, and how was their performance monitored?
eps
The BIRDS-III satellite used lithium-ion batteries. The battery performance was monitored in orbit using telemetry data, which included voltage, current, and temperature measurements.
148. Where can I find information about solar cells and batteries?
eps
Check the BIRDS GitHub: https://github.com/BIRDSOpenSource
149. What is a bypass diode for a solar panel, and how is inhibition handled for a solar cell with no bypass diode?
eps
To prevent over-discharge, blocking diodes are considered on the solar cell side. While solar cells have built-in bypass diodes, these are not intended for the solar cell itself. The internal bypass diode is used when two solar cells are connected in series. For the lower solar cells, at least one external bypass diode must be attached to the panel board. In some panel boards, the direction of series connection is reversed, and internal bypass diodes cannot be used. In such cases, two bypass diodes must be attached to the panel board. External bypass diodes can be confirmed in the circuit diagrams of the panel boards for the BIRDS project.