首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Preparing For Hyperseed MAC: An Observing Campaign To Monitor The Entry Of The Genesis Sample Return Capsule
Authors:PETER JENNISKENS  PAUL WERCINSKI  JOE OLEJNICZAK  GARY ALLEN  PRASUN N DESAI  GEORGE RAICHE  DEAN KONTINOS  DOUG REVELLE  JASON HATTON  RICHARD L BAKER  RAY W RUSSELL  MIKE TAYLOR  FRANS RIETMEIJER
Institution:(1) SETI Institute, 515 N. Whisman Rd., Mountain View, CA, USA;(2) NASA Ames Research Center, Moffett Field, CA, USA;(3) ELORET Institute, Sunnyvale, CA, USA;(4) NASA Langley Research Center, Hampton, VA, USA;(5) Los Alamos National Laboratory, Los Alamos, NM, USA;(6) U.C. San Francisco, San Francisco, CA, USA;(7) The Aerospace Corporation, El Segundo, CA, USA;(8) Utah State University, Logan, UT, USA;(9) The University of New Mexico, Albuquerque, NM, USA
Abstract:The imminent return of the Genesis Sample Return Capsule (SRC) from the Earth’s L1 point on September 8, 2004, represents the first opportunity since the Apollo era to study the atmospheric entry of a meter-sized body at or above the Earth’s escape speed. Until now, reentry heating models are based on only one successful reentry with an instrumented vehicle at higher than escape speed, the 22 May 1965 NASA “FIRE 2” experiment. In preparation of an instrumented airborne and ground-based observing campaign, we examined the expected bolide radiation for the reentry of the Genesis SRC. We find that the expected emission spectrum consists mostly of blackbody emission from the SRC surface (T∼ ∼2630 K@peak heating), slightly skewed in shape because of a range of surface temperatures. At high enough spectral resolution, shock emission from nitrogen and oxygen atoms, as well as the first positive and first negative bands of N2+, will stand out above this continuum. Carbon atom lines and the 389-nm CN band emission may also be detected, as well as the mid-IR 4.6-μm CO band. The ablation rate can be studied from the signature of trace sodium in the heat shield material, calibrated by the total amount of matter lost from the recovered shield. A pristine collection of the heat shield would also permit the sampling of products of ablation.
Keywords:Astrobiology  fireball  Genesis  meteor  reentry  sample return capsule  thermal protection system
本文献已被 SpringerLink 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号