ADEPT sounding rocket one (SR-1) flight experiment overview

Autor: Carl Kruger, Gregory T. Swanson, Paul Wercinski, Owen Nishioka, Stephen J. Battazzo, Soumyo Dutta, Alberto Makino, Shakib Ghassemieh, Bryan Yount, Ethiraj Venkatapathy, Brandon Smith, Chad Brivkalns, Alan M. Cassell, Shang Wu
Rok vydání: 2017
Předmět:
Zdroj: 2017 IEEE Aerospace Conference.
Popis: The Adaptable, Deployable Entry and Placement Technology (ADEPT) architecture represents a novel approach for entry vehicle design utilizing a high performance carbon-fabric to serve as the primary drag surface of the mechanically deployed decelerator. The ADEPT project team is advancing this decelerator technology via systems-level testing at the one-meter diameter (nano-ADEPT) scale. A subsonic aeroloads test (May 2015) and an arc-jet aeroheating test (Sept 2015) have already been completed. The initial system-level development of the nano-ADEPT architecture will culminate in the launch of a 0.7 meter deployed diameter ADEPT sounding rocket flight experiment named, SR-1. Launch is planned for August 2017. The test will utilize the NASA Flight Opportunities Program sounding rocket platform provided by UP Aerospace to launch SR-1 to an apogee over 100 km and achieve re-entry conditions with a peak velocity near Mach 3. The SR-1 flight experiment will demonstrate most of the primary end-to-end mission stages including: launch in a stowed configuration, separation and deployment in exo-atmospheric conditions, and passive ballistic re-entry of a 70-degree half-angle faceted cone geometry. ADEPT SR-1 will determine supersonic through transonic aerodynamic stability of the unique ADEPT blunt body shape with an open-back entry vehicle configuration.
Databáze: OpenAIRE