Far Horizons Project

h1. Far Horizons Project Requirements Document v1.0

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h3. 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_Questions_v1_0|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?

h3. 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 design and operation of the HAB shall comply with "FAR 101":http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr&rgn=div5&view=text&node=14:2.0.1.3.15&idno=14#14:2.0.1.3.15.4.

* *FHPR 4.2* The HAB will carry payloads to altitudes between 90 kft and 100 kft.

h3. 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 rocket engineering into the classroom, and anyone else interested in how rockets are tested can learn how to use it.

* *STSR 2.3* The STS documentation must cover the engine testing procedure from test stand setup, to running tests, and ending with stowing the test stand.

* *STSR 3.4* The STS shall be operated IAW the safety procedures which are outlined in Section 8 of the NAR testing manual.

* *STSR 4.3* The STS shall provide a fixed base on which to test model rocket motors.  

** *STSR 4.3.1* The test stand will remain stationary during motor firings.

** *STSR 4.3.2* The test stand components will not experience undo vibration during motor firings. 

* *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.

h3. 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:

* *STSR 5.1* High and low speed video capture of the tests from multiple angles.

* *STSR 5.2* Integrated ignition system so the test management software can control the entire test.

* *STSR 5.3* Additional measurements including:

** *STSR 5.3.1* The STS must meet the second part of the NAR testing manual requirement for casing temperature measurements and have a second thermocouple "3/4 of the way down the motor casing as measured from the nozzle end." "1":http://www.nar.org/SandT/docs/ST-MotorTestingManual.pdf

** *STSR 5.3.2* The STS must be able to record exhaust temperature vs time of Estes motors and transport that data to a laptop computer.

* *STSR 5.4* Higher resolution measurements.

Beyond Version 2.0 (Accommodation of):

* *STSR 5.5* High power commercial solid motors.

* *STSR 5.6* Small hybrid motors (on the thrust scale of high power commercial solid motors).

* *STSR 5.7* Larger thrust hybrid motors.

* *STSR 5.8* Small liquid engines.

* *STSR 5.9* Medium liquid engines.

* *STSR 5.10* Large liquid engines.

h3. Glossary

FHPR - Far Horizons Project Requirement

HAB - High Altitude Balloon