Primary Objectives and Success Criteria

  1. To develop and test an autonomous ocean recovery vehicle that will house a BalloonSat payload and is capable of surviving in near-space conditions.
  2. To develop and test an autonomous ocean recovery vehicle that will house a BalloonSat payload and autonomously return to a designated recovery location on the east coast of Oahu after being dropped into the ocean up to 5 miles offshore.
  3. To integrate the COSMOS platform to establish communications with mission control.
  1. The autonomous ocean recovery vehicle is successfully able to withstand all near-space condition tests.
  2. The autonomous ocean recovery vehicle is successfully able to propel and steer itself through the ocean to the designated recovery location from a drop point up to 5 miles offshore in typical spring weather conditions.
  3. The GPS and sensors are able to transfer engineering data to the GCS through COSMOS.
Primary Objective Performance Status
#1: Recovery Vehicle Progress 100%

Current status: Hull prototype manufactured and tested

#2: Autonomous Software Program Progress 100%

Current status: Successful ocean test of Ardupilot Mission Planner for autonomous mission and operations

#3: COSMOS Integration Progress 100%

Current status: COSMOS agents coded and successfully integrated into a temperature sensor onboard the recovery vehicle

Secondary Objectives and Success Criteria

  1. To graduate from the University of Hawaii at Manoa with a Mechanical Engineering degree in Spring 2021.
  2. To bring favorable publicity to the University of Hawaii at Manoa College of Engineering and Department of Mechanical Engineering.
  1. Passing ME 481 and ME 482.
  2. Favorable articles and features about UHABS-7 appear in the media.

Top-Level Requirements

Requirement IDObject NumberRequirement DescriptionPriorityRiskVerification MethodChild Requirements
SYS0011.1.1The recovery system shall autonomously return to a designated point onshore up to 5 miles off the east side of the Oahu coast.MandatoryMediumTestMECH001
ELEC004
SYS0021.1.2The recovery system shall be able to transmit and receive data and command signals from 5 miles offshore.MandatoryMediumTestELEC001
ELEC003
GCS001
GCS003
GCS004
SYS0031.1.3The recovery system shall remain fully functional after 60 minutes in near-space conditions.MandatoryMediumTestMECH009
MECH010
SYS0041.1.4The recovery system shall remain fully functional after an ocean impact at a speed of 15 feet per second.MandatoryMediumTestMECH002
MECH007
SYS0051.1.5The recovery system shall have data, location, and audio functionality after a terrestrial impact at a speed of 15 feet per second.MandatoryMediumTestMECH002
MECH008
SYS0061.1.6The recovery system shall remain fully functional after being exposed to ocean conditions for a specified time.MandatoryMediumTestMECH004
MECH005
MECH006
MECH011
SYS0071.1.7The UHABS-7 system shall use COSMOS for data management.MandatoryMediumTestELEC005
GCS002
SYS0081.1.8The recovery system shall be clearly visible and audible at the recovery location.MandatoryLowInspectionMECH003
MECH004
MECH005
MECH006
SYS0091.1.9The recovery system shall collect telemetry and mission data.MandatoryMediumTestELEC002
GCS001
GCS004

Mechanical Requirements

Requirement IDObject NumberRequirement DescriptionPriorityRiskVerification MethodChild Requirements
MECH0011.2.1The recovery vehicle shall be able to propel itself forward through the ocean in typical conditions with the weight of the payloadMandatoryMediumTestSYS001
MECH0021.2.2The recovery vehicle shall have a detachable parachute that slows the descent of the recovery vehicle to 15 feet per second when fully deployed.MandatoryMediumTestSYS004
SYS005
MECH0031.2.3The recovery vehicle shall have an audible and waterproof location beacon capable of functioning continuously for 24 hours.MandatoryMediumTestSYS008
MECH0041.2.4The recovery vehicle shall be clearly marked with contact information that will still be visible after extended exposure to saltwater and sunlight.MandatoryLowInspectionSYS006
SYS008
MECH0051.2.5The recovery vehicle shall have an American flag that will still be visible after extended exposure to saltwater and sunlight.MandatoryLowInspectionSYS006
SYS008
MECH0061.2.6The recovery vehicle shall be painted in a waterproof, highly visible color that will not be affected by extended exposure to saltwater and sunlight.MandatoryLowInspectionSYS006
SYS008
MECH0071.2.7The mechanical subsystem shall be able to withstand an ocean impact at a speed of 15 feet per second.MandatoryHighTestSYS004
MECH0081.2.8The mechanical subsystem shall be able to protect the payload to withstand a terrestrial impact at a speed of 15 feet per second.MandatoryHighTestSYS005
MECH0091.2.9The mechanical subsystem shall survive in near space temperatures for 60 minutes.MandatoryMediumTestSYS003
MECH0101.2.10The mechanical subsystem shall survive in near space pressures for 60 minutes.MandatoryMediumTestSYS003
MECH0111.2.11The mechanical subsystem shall survive in ocean conditions for a specified time.MandatoryMediumTestSYS006

Electrical Requirements

Requirement IDObject NumberRequirement DescriptionPriorityRiskVerification MethodChild Requirements
ELEC0011.3.1The electrical subsystem shall be able to receive and carry out commands as given by the GCS.MandatoryMediumTestSYS002
ELEC0021.3.2The electrical subsystem shall be able to collect data at specified intervals throughout the duration of the mission.MandatoryMediumTestSYS009
ELEC0031.3.3The electrical subsystem shall be able to transmit data at specified intervals throughout the duration of the mission.MandatoryMediumTestSYS002
ELEC0041.3.4The onboard electrical subsystem shall sufficiently power all electronic components onboard the recovery system for the duration of the mission.MandatoryMediumTestSYS001
ELEC0051.3.5The electronic components shall be compatible with COSMOS.MandatoryMediumTestSYS007

Ground Control Station Requirements

Requirement IDObject NumberRequirement DescriptionPriorityRiskVerification MethodChild Requirements
GCS0011.4.1The GCS shall receive all sensory, imagery, and GPS data throughout the duration of the mission.MandatoryHighTestSYS002
SYS009
GCS0021.4.2The GCS shall use COSMOS to manage mission data.MandatoryMediumTestSYS007
GCS0031.4.3The GCS shall transmit commands and tasking to the recovery system.MandatoryMediumTestSYS002
GCS0041.4.4The GCS shall have a transmission range of 5 miles.MandatoryLowTestSYS002
SYS009