Impulsive Hyperbolic Injection from a Circular Earth Orbit

Description:Determines the characteristics of the single impulsive maneuver required to transfer a spacecraft from an initial circular Earth park orbit to a departure hyperbola.
Filename:demo_hyper1.zip
ID:9462
Author:C. Deagle, Jr.
Downloaded file size:337,793 bytes
Size on calculator:30 KB
Platforms:Prime  
User rating:Not yet rated (you must be logged in to vote)
Primary category:Science
Languages:ENG  
File date:2022-09-17 04:20:28
Creation date:2022-10-16
Source code:Included
Download count:84
Version history:2023-05-28: Added to site
Archive contents:
  Length      Date    Time    Name
---------  ---------- -----   ----
    30242  2022-10-16 08:05   demo_hyper1.hpprgm
     3051  2022-09-17 04:20   demo_hyper1.html
    14963  2022-10-16 08:04   demo_hyper1.txt
   357110  2013-12-15 16:19   hyper1_matlab.pdf
---------                     -------
   405366                     4 files
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