Title : 
2001 Mars Odyssey payload suite - The long, arduous journey to launch
         
        
            Author : 
Kloss, Carl, Jr. ; Girard, Timothy J. ; Heinsohn, Greg ; Schulz, Cindy K.
         
        
            Author_Institution : 
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
         
        
        
        
        
            Abstract : 
The 2001 Mars Odyssey spacecraft was successfully launched from the Cape Canaveral Air Force Station (CCAFS) on April 7, 2001. The payload suite consists of a gamma-ray spectrometer, a thermal emission imaging system, a Martian radiation environment experiment, and a high energy neutron spectrometer. The payload development model was based on the "faster, better, cheaper" Mars 98 Project (an orbiter and lander for $96M). Development of the payloads and assembly, test, and launch operations (ATLO) had significant challenges due to the low-cost nature of the project. Prior to payload deliveries, NASA imposed Red Team payload reviews to mitigate risk. Final payload integration occurred just two months before launch. Post-launch checkout was successfully completed three months after launch. This paper discusses the payload objectives, designs, procurement costs/philosophy, development and test challenges, lessons learned, and reports on the in-flight checkout.
         
        
            Keywords : 
aerospace testing; economics; reviews; space vehicles; 2001 Mars Odyssey spacecraft; NASA; Red Team payload reviews; assembly; gamma-ray spectrometer; high energy neutron spectrometer; launch operations; payload integration; payload suite; post-launch checkout; procurement costs; radiation environment experiment; test challenges; thermal emission imaging system; Assembly; Mars; NASA; Neutrons; Optical imaging; Payloads; Procurement; Space vehicles; Spectroscopy; Testing;
         
        
        
        
            Conference_Titel : 
Aerospace Conference Proceedings, 2002. IEEE
         
        
            Print_ISBN : 
0-7803-7231-X
         
        
        
            DOI : 
10.1109/AERO.2002.1036836