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Grants and Contracts Details
Description
Development of Kentucky Aboard Norwegian GHOST (Sat) (KANG(S))
1. Objective
The objective of this project is to conduct a successful deployment of the KRUPS capsule and
corresponding communication femtosats from a sounding rocket to validate payload
instrumentation, rocket systems, and data collection technology. The test will assess the capsule’s
performance during suborbital flight and ensure that the payload functions correctly under the
extreme conditions of launch, ascent, and descent. The mission aims to gather scientific and
performance data, which will be used to evaluate the efficacy of KRUPS communication,
telemetry systems, and payload survival.
2. Scope of Work
The scope of work for this project includes all activities required for the preparation, execution,
launch and post-launch activities surrounding the sounding rocket test. This includes pre-launch
preparations, the launch itself, and post-launch data retrieval and analysis, ensuring the mission
objectives are met efficiently and safely. Following guidelines of this NASA program and
objectives of the National Space Grant program, this is a design and operations project led by a
team of engineering students.
A. Pre-Launch Phase
1. Design and Planning: The team will plan all the detailed designs of the capsules and femtosats,
ensuring that they meet all mission requirements. This includes confirming the rocket''s flight
parameters (altitude, velocity, flight duration) and ensuring compatibility between the payload and
the rocket''s instrumentation. Additional steps include collaboration with technical staff at NASA
Wallops to review environmental factors such as weather conditions and how they may affect
launch windows and mission safety. Finally, we will also work on establishing a comprehensive
mission timeline, from final assembly to launch day, covering every milestone.
2. Safety and Compliance: We will also work with NASA Wallops staff and other relevant
authorities to ensure all operations meet national and international safety regulations, such as those
set by the Norwegian Space Center and international space law. We will submit risk assessments
and mitigation plans for hazards, such as failure to deploy, ensuring robust contingency protocols
are in place. We will review safety procedures with the NASA team through monthly design review
meetings.
3. Ground Testing: As part of the test, we will conduct comprehensive pre-launch testing of the
KRUPS and femtosat systems, including telemetry checks to ensure accurate data transmission
during flight. The heat shield system will be tested for adequate protection from the environment.
Environmental stress tests on the payload will ensure that it can survive the intense vibrations and
extreme temperatures during launch and re-entry. We will review all system health checks,
troubleshooting any discrepancies before integrating the capsule to the rocket.
B. Launch Phase: During launch, we will perform a final set of systems checks, including
telemetry, to ensure that all components are operating within safe parameters. We will monitor
health of the capsule in real-time using ground-based telemetry systems, tracking its flight path
and recording essential data such as altitude, velocity, and payload status.
C. Post-Launch Phase: We will recover scientific data through telemetry transmission during
flight and from data stored on the payload. We will retrieve the payload (if recovery systems are
in place), assess its condition, and extract all experimental data. Perform a full analysis of the flight
data, evaluating how well the capsule performed against pre-launch predictions. This includes
examining any anomalies, deviations from planned flight paths, or data collection issues. We will
compile a detailed report summarizing all phases of the mission, including pre-launch preparation,
launch execution, and post-launch analysis. This report will include flight performance data,
system diagnostics, payload results, and lessons learned.
3. Personnel
Dr. Savio Poovathingal will serve as PI on the project and provide leadership of the student team
to meet the overall project requirements and KY Space Grant Consortium objectives. The project
will support an hourly undergraduate student to serve as team lead. A senior design team will
contribute to mechanical design, avionics, and software / hardware engineering. Additional
Engineering faculty will provide guidance as needed.
Status | Active |
---|---|
Effective start/end date | 10/1/24 → 1/31/25 |
Funding
- National Aeronautics and Space Administration
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Projects
- 1 Active
-
NASA Kentucky Space Grant Consortium Program 2020-2024
Martin, A. (PI), Renfro, M. (CoI) & Smith, S. (CoI)
National Aeronautics and Space Administration
2/4/20 → 2/3/25
Project: Research project