Difference between revisions of "Aquila"
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Aquila (previously 'Condor') is the second stage of Griffin 1, CUSFs first attempt to cross the Karman line. It is powered by a Cesaroni Pro-98 motor, has a bistable fin system, and is equipped with a hypersonic recovery system. CUSF intend to launch Aquila for testing of the recovery system in 2022. | Aquila (previously 'Condor') is the second stage of Griffin 1, CUSFs first attempt to cross the Karman line. It is powered by a Cesaroni Pro-98 motor, has a bistable fin system, and is equipped with a hypersonic recovery system. CUSF intend to launch Aquila for testing of the recovery system in 2022. | ||
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[https://colab.research.google.com/drive/1rUCjscI7ql-d8v7F-hSEKYIfJihA8GnZ?usp=sharing Aquila Stability Python Notebook - October 2021] | [https://colab.research.google.com/drive/1rUCjscI7ql-d8v7F-hSEKYIfJihA8GnZ?usp=sharing Aquila Stability Python Notebook - October 2021] | ||
== Thermal Modelling == | == Thermal Modelling == | ||
[https://drive.google.com/file/d/1FSWIPIXe7zcrkjioAzZGbWGs958NZK1x/view?usp=sharing Aquila Thermal Analysis - October 2021] | [https://drive.google.com/file/d/1FSWIPIXe7zcrkjioAzZGbWGs958NZK1x/view?usp=sharing Aquila Thermal Analysis - October 2021] | ||
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== Structural Analysis == | == Structural Analysis == | ||
[https://drive.google.com/file/d/1m-FBpQ04GnAARqVHANoUYtXHb9HFTd_-/view?usp=sharing Aquila Structural Analysis] - December 2021 | |||
[https://drive.google.com/file/d/1eVyk5nxJv5zGCBUd-P7BJdI-admP_hoD/view?usp=sharing Aquila full structural CAD] - January 2022 | |||
Latest revision as of 03:28, 9 February 2023
Aquila (previously 'Condor') is the second stage of Griffin 1, CUSFs first attempt to cross the Karman line. It is powered by a Cesaroni Pro-98 motor, has a bistable fin system, and is equipped with a hypersonic recovery system. CUSF intend to launch Aquila for testing of the recovery system in 2022.
History
Griffin 1 was conceived in early 2020, but specific work on Aquila did not begin until early 2021, when Barty Wardell was appointed Aquila PM after the March 2021 AGM. Following his appointment, there was a period of very rapid development of the Aquila aero in April 2021, partially based off of Martlet 4, but the stability had to be 2 directional due to the nature of the recovery system. After this period of rapid design at the end of April, development has slowed for exam season, with only some design review and documentation taking place over summer.
Hypersonic recovery system and Deployment - Daedalus
Parachute analysis from Michaelmas - November 2020
Plan for Lent and Easter 2021 - February 2021
Parachute analysis procedure and notes collated into a mini textbook - March 2021
Feasibility of using CFD - March 2021
Initial deployment system design - March 2021
Hemisflo drogue design specification and analysis - April 2021 (Latest design for Hemisflo Drogue)
Hemisflo drogue design (just the numbers without the justification) - April 2021
Deployment system design - August 2021
Deployment System Pressure Analysis - October 2021
Aerodynamics and Aeroelastic Modelling
Summary of flutter in rocket fins - April 2021
Aquila aerodynamic analysis principles - August 2021
Aquila aerodynamic specifications - August 2021
Aquila Buffet and Drag Ascent Analysis - October 2021
Aquila Fin Ring Analysis - October 2021
Aquila Skin Structural Analysis - October 2021
Aquila Aeroelastic Fin Analysis - October 2021
Aquila Structure STEP File - October 2021
Aquila Aerodynamics and Structures Python Scripts - October 2021
Aquila Stability Python Notebook - October 2021
Thermal Modelling
Aquila Thermal Analysis - October 2021
Aquila Thermal Design Solution - November 2021
Structural Analysis
Aquila Structural Analysis - December 2021
Aquila full structural CAD - January 2022