NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Test Vehicle Forebody Wake Effects on CPAS ParachutesParachute drag performance has been reconstructed for a large number of Capsule Parachute Assembly System (CPAS) flight tests. This allows for determining forebody wake effects indirectly through statistical means. When data are available in a "clean" wake, such as behind a slender test vehicle, the relative degradation in performance for other test vehicles can be computed as a Pressure Recovery Fraction (PRF). All four CPAS parachute types were evaluated: Forward Bay Cover Parachutes (FBCPs), Drogues, Pilots, and Mains. Many tests used the missile-shaped Parachute Compartment Drop Test Vehicle (PCDTV) to obtain data at high airspeeds. Other tests used the Orion "boilerplate" Parachute Test Vehicle (PTV) to evaluate parachute performance in a representative heatshield wake. Drag data from both vehicles are normalized to a "capsule" forebody equivalent for Orion simulations. A separate database of PCDTV-specific performance is maintained to accurately predict flight tests. Data are shared among analogous parachutes whenever possible to maximize statistical significance.
Document ID
20170004357
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Ray, Eric S.
(Jacobs Technology, Inc. Houston, TX, United States)
Date Acquired
May 3, 2017
Publication Date
June 5, 2017
Subject Category
Aircraft Design, Testing And Performance
Aerodynamics
Report/Patent Number
JSC-CN-38971
Meeting Information
Meeting: AIAA Aerodynamic Decelerator Systems Technology Conference
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available