Question 6 Description of Research Project

0305-EX-PL-2014 Text Documents

Texas A&M; University AggieSat Lab

2014-04-07ELS_147774

Form 442 Question 6 Exhibit: Nature and Necessity of Research

Description

Our research is in support of sensor development with the National Aeronautics and
Space Administration’s Johnson Space Center (NASA JSC), the test bed for which will
be a microsatellite developed, constructed, and operated by AggieSat Lab.

An experimental license has been granted to AggieSat Lab (File #: 137-EX-ML-2012,
Call Sign: WG2XFJ) for the purpose of one-way High Data Rate transfers from our
satellite to our ground station. The purpose of this submission is to seek frequency
authorization to transmit telemetry and station-keeping data from the spacecraft back to
the ground on bands and equipment different than those authorized by the
aforementioned license. A separate license request will be submitted for our ground
station equipment.

This satellite is designed to fly a prototype GPS receiver, developed by NASA JSC, and
take navigation data to determine the usefulness of using such a receiver for navigating
with orbital spacecraft. Results of this project and further development have a direct
impact on NASA’s planned navigational aids for the Space Station operations, the Multi-
Purpose Crew Vehicle (MPCV), and other commercial spacecraft in development.

NASA approached Texas A&M University to find a student group to develop this
payload. The goals of this project are to provide useful engineering data to NASA JSC
concerning this GPS receiver and educate university students in the design and operation
of spacecraft.

Necessity of Research and Inadequacy of Current Facilities

This project requires navigation data to be taken in the space environment to characterize
the ability of GPS to perform at speeds and altitudes orders of magnitude greater than
typical Earth based applications. This requirement facilitates the need for a satellite
platform and a satellite platform requires facilities capable of proper distance
communications for operation.

The choice to use the bands requested in form 442 in the 144 MHz and 440MHz bands
was driven by the desire to utilize amateur radio hardware to control the spacecraft, due
to the limited resources available to the lab.

Our spacecraft for this mission is a 24x24x11 inch box, ~ 110 lbs in weight. The first
part of the spacecraft communications system will consist of two Kenwood TH-D72A
radios, each operating on one of the frequency ranges applied for in form 442 if granted.
The second piece of spacecraft communications hardware is a Digi XTend-PKG radio
operating on the 915 MHz band. (A custom RFIC unit, operating under the experimental
license grant mentioned in the second paragraph will also be used.)


The 144 MHz band frequencies will be used for the spacecraft command uplink, and the
440 MHz frequencies will be used as the spacecraft identification beacon and an
alternate/emergency downlink unit. The Digi XTend in the 915 MHz band operates on
Frequency Hopping Spread Spectrum protocol, and will be used exclusively for
spacecraft crosslink communication with our partner satellite from the University of
Texas. Licensing for the University of Texas radio systems is to be handled by their
program separately from ours. The custom RFIC unit will be used solely as high data
rate downlinking transmitter as specified by the license, and will transmit one way from
the spacecraft to our College Station, Texas ground station upon ground command.

Our first course of action was to ask for usage of NASA’s extensive array of existing
communications links. We were denied permission to use these links as they are needed
to support high priority national programs and are also directly linked to the safety of
manned spaceflight operations.

Our lab currently has a ground station capable of spacecraft tracking and UHF/VHF
communication. The license application for use of this station with the above described
satellite operations will be submitted in an application to follow this one.



Document Created: 2014-04-07 16:04:57
Document Modified: 2014-04-07 16:04:57

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