Launch S801 Prereport

General Launch Information:

Date: March 2nd
Departure Time:

  • Ham Shack: 04:45

Launch Site: Spangle
Landing Site: Palouse

Post Flight Status: Partial Mission Success

Goals and Success Criteria

Prior to launch the project management creates specific and measurable success criteria for the launch. In addition each team establishes a set of goals. Team goals are considered secondary to meeting the Mission Success criteria.

Project Success Criteria

Minimum Success

  • Payload recovered within 1 week of launch

Mission Success

  • Payload recovered within 2 days of launch
  • Collect temperature data as a function of time during the entire flight
  • Capture and store 100 or more digital still pictures
  • Collect and store at least 50% of the tracking packets containing accurate position and altitude data real time during the flight
  • Archive all raw flight data (GPS packets, science data, pictures, video) on VAST computer in Ham Shack within 24 hours of recovery
  • Each team posts lessons learned on wiki (Post Flight Report) within 1 week of launch date

Full Success

  • Payload recovered within the same day of launch
  • Collect temperature data as a function of time during the entire flight
  • Collect pressure data as a function of time during the entire flight
  • Capture and store 200 or more digital still pictures
  • Collect and store at least 80% of the tracking packets containing accurate position and altitude data real time during the flight
  • Reach peak altitude of at least 90,000 ft
  • Archive all processed/calibrated flight data (GPS packets, science data, pictures, video) on VAST computer in Ham Shack within 1 week of recovery

Team Launch Objectives

Science/Instrumentation Objectives

  • New camera - pictures every ten seconds for entire flight
  • Old system - all sensors reading and storing accurate data

Communication Objectives

  • To receive Big Red Bee packets throughout the flight but importantly at the very end for maximum GPS precision
  • To receive the majority of the Microtrak packets to be able to track and reconstruct the flight
  • To hit digi-peaters with the majority of microtrak packets and be able to track the flight online
  • To effectively use the radios for both data and voice simultaneously

CnDH Objectives

  • Mission Failure
    • Loss of payload or
    • destruction of payload or
    • no data recovered
  • Minimal success
    • recover payload intact
    • powers on
    • GPS data recorded and recovered
    • Invalid data from sensors
    • PIC AXE communication with ARM7
  • Moderate success
    • Valid sensor data
      • Pressure
  • Full success

Note: Valid data consist of calibrated and verified data to atmospheric models.

Ground Station Objectives

  • Mobile Unit:
    • Log all the bus packets
    • Test the new GPSD2COM software with 2 new mapping programs
      • Vast Dashboard running Microsoft Mappoint
      • Other software test
    • Pictures!!
  • Stationary Unit (Ham Shackians):
    • Log all the balloon packets via radio (fall back will be [aprs.fi])
    • Pictures!!
    • Test out the new C++ GERTTS in real time

Structures Objectives

  • All capsules return in a reusable condition
  • Less than 30 minutes of set-up time on site
  • All capsules maintain sufficient thermal integrity to ensure power systems remain functional
  • All critical components return in a reusable condition

Roles and Responsibilities

Each team member volunteers for a role on launch day. There are two catagories of roles, project level roles and team level roles. The project level goals include: Head Flight Planner, Launch Coordinator, Tracking Coordinator, Recovery Coordinator, and Communication Specialists. Team level roles include: Photographer, Head Note Taker and other specialized roles specific to the team.

Management Roles

Flight Planner Austin Howard
  • File NOTAM with FAA
  • FAA field contact
  • Manage launch inventory
Launch Coordinator Justin Schlee
  • Coordinate launch efforts (located at launch site)
  • Launch countdown
  • Manage integration/launch checklist
Tracking Coordinator Jasper Nance
Evan Hart
  • Coordinate tracking efforts
  • Ground Station Manager
  • Archive all flight data real time
Recovery Coordinator
  • Run predicts/define launch location
  • Coordinate recovery efforts (located with mobile tracking vehicle)
  • Coordinate photograph/video the landing site
Communications Specialists Alex Odom (HamShack)
Matthew VavRosky (Steptoe?)
Austin Howard (Bus?)
  • One for each radio (1 at each location)
  • Know how to work radio/computers

Team Roles

Communications
  • Note Taker
  • Photographer
  • Radio
Controll &
Data Handling
  • Note Taker
  • Photographer
  • Integrator
  • Micro controller Engineer
  • Supplies
Science/Instrumentation
  • Note Taker - TBD (Date Dependent)
  • Photographer - TBD (Date Dependent)
Ground Station Cliff Murphy (pics-Bus)
?? (notes-Bus)
Alex Odom (notes-HamShack)
Evan Hart (pics-HamShack)
  • Note Taker
  • Photographer
Structures
  • Liaison officer
  • Rigging
  • Capsule Assembly

Launch Procedures

Prior to launch the teams create a collaborative procedure for assembling the payload and checking for critical functionality. A final launch checklist is also used to confirm that all systems are ready for launch.

  1. Begin filling the balloon
  2. Assemble capsules
    • Turn on camera and system located in the high school capsule
    • Secure attachments to batteries
    • Verify data is being received
    • Verify connections between devices/batteries
    • Verify valid data being received on datalogger
  3. Attach harnesses to capsules
  4. Attach parachute and capsules to balloon
  5. Attach cut-down system (inactive for this launch (March 2nd, 2008)
  6. Final verification of signal transmission
  7. Lift-off

Final Launch Checklist

Tracking and Recovery Plan

We will have two tracking stations set up. Both will be mobile units. The Lima unit will drive to the launch site and set up the balloon for launch and confirm functionality prior to launch. The Romeo unit will situate its-self at the highest spot as close as possible to the predicted landing zone. Prior to release, Lima will contact Romeo (via cell phone) and confirm that Romeo is ready to receive. Upon release Lima will pack up and drive furiously with great abandon to the location of Romeo. Upon balloon burst, indicated by a rapid decrease in reported altitude, Romeo will pack up the BBQ and prepare to move to the expected landing site.

Lima and Romeo form up to create Vandal. Vandal packs up the capsule and returns to campus.

HamShack School Bus Truck Jasper Mobile CNR SUV
Moscow
medium.jpg
Launch Site
schoolbus.jpg
Launch Site
small.jpg
Launch Site
jaspermobile.jpg
Step Toe Butte
small.jpg
Personnel Personnel Personnel Personnel Personnel
Equipment Equipment Equipment Equipment Equipment
  • Kenwood D710
  • Cookies!
  • Kenwood D700 (Dual Band)
  • Inverter(s)
  • Linksys WRT54G Router/GPS
  • Multimeter
  • Helium Tanks
  • Table
  • F6 + Antenna
  • Inverter(s) (Jaspers)
  • F6 + Antenna
  • 2 Jaspertops
  • Inverter(s)
  • D7 (Dual Band)

Radio Frequencies

VAST uses amateur radio to track the payload in real time and transmit telemetry data from the balloon to the mobile ground units.

Audio Communications:

Primary Frequency: 146.550Mhz (Simplex)
Secondary Frequency: 146.820Mhz (Moscow Mt Repeater), 147.240Mhz (Mica Mt Repeater)

Location Operator Callsign Unit RF Power
HamShack Alex Odom KE7HLM Kenwood D710 50W
The Bus Chris Walker KE7PHE Kenwood D700 50W
Jasper Mobile Jasper Nance KE7PHI Kenwood Fd F6A*2 5W
CNR-SUV Cliff Murphy KE7PHG Kenwood D700/Yaesu FT-60R 50W/5W
Steptoe W7UQ Radio Club KE7CJL/KE7MTF/KE7MT-? Kenwood D7/HTs 5W-50W

Transmitters:

Unit Use Callsign Frequency Data Time Interval RF Power
Microtrak 8000 FA tracking KE7PHI-1 144.390Mhz APRS 113 sec 8W
Microtrak 300 + MicroAmp tracking KE7JWW 144.390Mhz APRS 87 sec (offset by 60) 10W
Big Red Bee + Amp precision tracking KE7PHI-2 441.050Mhz pseudo APRS 10 sec 1W

Receivers:

Unit Freq: Pri/Sec Computer Software Antenna
APRS.fi iGates HamShack PC GERTTS
Kenwood D710 441.050Mhz HamShack PC MapPoint/GERTTS ??

Flight System

Parachute / Balloon Info

  • Parachute Type: Rocketman R12C
  • Balloon Type: Latex
  • Size: 1500 g

Target Flight Rates

  • Targeted Free Lift: 1.5-2 lbf
  • Average Target Ascent Rate: 1200 ft/min
  • Average Target Descent Rate: 2000 ft/min
  • Target Peak Altitude: 100,000 ft

Payload

BC 1 - Waldo

MCC 3- Twiddle Dee

Waldo.jpg
twiddle_dee.JPG

Contents:

  • Rabbitt-GPS
  • Hobo 1
    • Location: Bottom Shelf
    • Internal and External Temperature Readings Taken

Contents:

  • 2 x Microtrack-GPS-Battery Pack
  • Big Red Bee with Amplifier
  • Camera
Mass: 616g (empty) Mass: 382g (empty)

Trajectory/Weather Predictions (Prediction Tutorial)

VAST uses multiple trajectory prediction tools including an online tool. Weather forecasts are also used for planning and logistics. Launches are postponed if surface winds are dangerously high or if there is too much precipitation. The wind speed in the jet stream is also an important consideration. If winds are too high, the launch team will have to drive long distances to avoid forested landings in northern Idaho.

Risk Analysis

Each team summarizes all failure modes and the steps taken to mitigate system failures. Teams highlight failure modes that are single point failures, dependent failures, and failures that effect other systems. Failures are rated by likelihood and consequence (rated from 1-5, where 1 represents low and 5 high). Use this image as a guide to mitigating risk.

Systems

Failure Mode Description Likelihood Consequence Risk (R=L*C)
Package comes in contact with aircraft 1 5 5

Science

Failure Mode Description Likelihood Consequence Risk (R=L*C)
Camera Failure 2 2 4

C&DH

Failure Mode Description Likelihood Consequence Risk (R=L*C)
Example 1 1 1

Comm

Failure Mode Description Likelihood Consequence Risk (R=L*C)
Early Battery Discharge 1 4 4
Amplifier overheating 2 5 10
Last GPS packets missed 2 3 6

Structures

Failure Mode Description Likelihood Consequence Risk (R=L*C)
Thermal Failure 3 8 24
Capsule/Rigging Integrity Dissipates 2 10 20

Ground Station

Failure Mode Description Likelihood Consequence Risk (R=L*C)
Example 1 1 1

Validation/Verification

Each team posts a summary of all relevant system testing including description of test and outcomes.

Systems

Control and Data Handling

Communication

Science

New camera was spin tested, pictures resulting were of decent quality. Internal timer tested.

Structures

MCC 3- Twiddle Dee was drop tested with no major damage to the capsule or components.
New Rigging was fitted to MCC 3- Twiddle Dee.

Ground Station

FAA/Sheriff Information

A NOTAM is filed the day before launch. In addition a fax is sent to the surrounding sheriffs offices to inform them of our activities. The relevant details of the launch are summarized in the link below.
NOTAM
Sheriff Fax

Contacts

Leaders Contacts
Sheriff Contacts
FAA Contacts

Checklists

Personal