Boston University Daniel TaylorNima Badizadegan R. Terry BlackPantelis Thomadis

Mission 1: Communications Determine packet loss in near-space environment – Measuring rate of packet loss at varying altitudes Proof of concept for status beacon – Status beacon will begin when BUSAT is launched, contains vital status information – Important part of communications system

Mission 2: Magnetometer Testing magnetometer in different thermal environments Determine three orthogonal magnetic field vectors Determine how well the magnetometer will work near radio and power systems – Large source of interference

SHOT II / UN-7 Connection Communications system test – Packet loss – Near space environment – Proof of concept for beacon Magnetometer – Thermal testing – Stored data can be used for calibration in the future – Same setup as on BUSAT

SHOT II Design – Block Diagram

SHOT II Design – Software No software needed for radio – Beacon set up automatically Microcontroller software: – Read data from Magnetometer every 42 seconds – Data stored in EEPROM (512 bytes total) – 113 data points per axis

SHOT II Design – Mechanical

SHOT II Test Procedure Chase balloon around with handheld Yagi antenna – Receive and record any packets received from the beacon, can be checked for error rate Magnetometer records data automatically – One sample every 62 sec – EEPROM can be read when the payload is recovered

Expected Data Magnetometer: 113 data points for each axis – Data comparable to IGRF data – Should indicate that magnetometer correctly reads magnetic field (with error) over large temperature range Communications: packet loss data – Able to decode and read packets on the ground – Low packet loss (75% received)

Test Results Structural Tests – Payload survived all tests with minimal damage Functional Tests – Testing completed with expected results – Successfully retrieved magnetometer data – Communications received 80% of packets transmitted