Far Horizons Project Requirements Document v1.0¶

• Far Horizons Project Requirements Document v1.0
  • • Introduction
    • Technical Requirements
    • Project Requirements
    • Future V2.0 Requirements
    • Glossary

Introduction¶

The requirements list matches up to the Initial Questions in step one of the Systems Engineering process as shown below. Each requirement is labeled with FHPR (Far Horizons Project Requirement), followed by the number of the initial question that the requirement corresponds to, followed by a dot and then the ID number of the requirement.

• FHPR 1.x - Why are we making this?
• FHPR 2.x - Who is this for?
• FHPR 3.x - How will this be used?
• FHPR 4.x - What features does it need to have (now)?
• FHPR 5.x - What features does it need to have (later)?
• FHPR 6.x - What are the legacy requirements?
• FHPR 7.x - Who's going to build this?
• FHPR 8.x - How many do we want to make?
• FHPR 9.x - What is the budget?
• FHPR 10.x - What is the timeline?
• FHPR 11.x - What waste products will be produced by the manufacture and/or operation of this?

Technical Requirements¶

Technical requirements are those requirements which include measurable performance values. Each technical requirement should be verified through testing to ensure the design meets the requirement.

• FHPR 3.1 The HAB must be able to carry scientific and engineering payloads to a "near space environment" and return the payloads safely.
  • FHPR 3.1.1 Individual payload modules must weigh 6 lbs or less.
  • FHPR 3.1.2 Total launch weight must be 12 lbs or less.
• FHPR 3.2 The HAB must be able to withstand the near space environment (TBD - fill in min temperatures, pressures, and max radiation levels as sub-requirements).

• FHPR 4.1 The HAB will carry payloads to altitudes between 90 kft and 100 kft.

• FHPR 6.1 The design and operation of the HAB shall comply with FAR 101.

Project Requirements¶

Project requirements are the remaining requirements which are not tied to specific performance values.

• FHPR 2.1 The HAB must be well documented so as to meet the needs of open source spaceflight designers who will design and build High Altitude Balloons (at Adler and elsewhere).
• FHPR 2.2 The HAB documentation and procedures must be complete enough that Adler operators, students and educators who want to bring near space missions into the classroom, and anyone else interested in running near space missions.
• FHPR 2.3 The HAB documentation must cover the the development, setup, launch, and recovery of the HAB.

• FHPR 4.2 The HAB documentation shall include safety guidelines for launch and recovery.
• FHPR 4.3 The HAB will broadcast a tracking signal to facilitate recovery.
• FHPR 4.4 The HAB will include a parachute or similar descent control system to provide a soft landing.

• STSR 7.1 All STS design documentation must be open and complete enough so that ANYONE, without necessarily a technical education in rocketry, propulsion, or engineering, would be able to build and operate the test stand.

• STSR 8.1 The design of the STS must enable the completion of at least one operational test stand.
• STSR 8.2 Whenever and wherever possible, considerations should be made so that the design of this STS can be used as a kit in the future.

• STSR 9.1 The cost of the first operational STS must not exceed $200 excluding "consumables" and tools.

• STSR 10.1 If at all possible, the STS should be completed within 3 months of formal launch as an exercise in agile design.

• STSR 11.1 Disposal of the spent Estes motors should conform to all local, state, and federal guidelines.
• STSR 11.2 Electronic waste items, including batteries and circuit boards, must also be disposed of according to all local, state, and federal guidelines.
• STSR 11.3 If the frame of the STS is damaged beyond repair during operation, proper disposal/recycling guidelines must be followed for the materials used in its construction.
• STSR 11.4 Wherever possible, the STS design should make it as easy as possible to replace components which are consumable or relatively easy to damage.

Future V2.0 Requirements¶

These are for reference only so that future features can be accommodated in the current design where practical.

Version 2.0 and beyond:

• FHPR 5.1 Controlled descent system (guided landings using parafoil kite to either hit or avoid landing sites)
• FHPR 5.2 Live two-way telemetry (or command & control) and the ability to receive live experiment and operations data
• FHPR 5.3 Stabilized platform system (Adler is making progress on this one)
• FHPR 5.4 Alternative balloon configurations (zero-pressure, super-pressure balloons)
• FHPR 5.5 Alternate lift gasses (Adler uses helium right now)
• FHPR 5.6 A structure to hold the balloon during filling operations and to automatically stop the filling operation for the desired lift

Glossary¶

FHPR - Far Horizons Project Requirement
HAB - High Altitude Balloon