Overview
The payload for the Space Shot engages with the local community and collects data on the rocket flight.
Primary scope: Outreach payload + heat mapping of nose cone
Requirements (as of 9/5/2018, not firm)
Outreach Payload
- TBD
Instrumentation Package
- Data Type
- Temperature
- at least 1 under NC tip, at least 4 on surface
- at least 2 on the cylindrical walls
- Load
- Chutes
- strain gauges on tubes
- Accelerometer
- Microphone
- Piezos
- etc.
- Temperature
- Data Rate & Storage
- Temperature 10-100Hz
- at least 1 under NC tip, at least 4 on surface
- at least 2 on the cylindrical walls
- Load - 100 Hz
- Accelerometer - O(10kHz)
- Microphone
- Piezos
- etc.
- Temperature 10-100Hz
- Hardware Form Factor
- Does not affect recovery system deployment
- Thermocouple map onto nose cone
- Interface w/ Structures for NC geometry
- Length limit 10"
- Set by NC space for 1st-stage only descope
- TBD architecture of S2 with IP
- Operational
- 2 hours of on-pad life
- Data Storage
- Thermal
- Battery life
- Acceptable sensor drift
- Remote Arming via Pyxida
- Relay data to Pyxida
- Integration time < 1/2 hour
- 2 hours of on-pad life
Tests Based on Requirements
Requirement 1:
- Bench test w/ sensors running
- Life test: 2 hrs. of "on pad" simulated with hardware
- Data Storage
- Thermal
- Battery life
- Acceptable sensor drift
- Remote Arming
Requirement 2:
- Bench test & life test (see req. 1)
Requirement 3:
- CRIMP
Requirement 4:
- Life test (see req. 1)
- CRIMP