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(HP-65) Analytic solution for low thrust out of ecliptic mission design
08-03-2023, 12:43 PM
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(HP-65) Analytic solution for low thrust out of ecliptic mission design
A small challenge for so inclined:

the attached PDF is an extract (pgs. 6-7) from AIAA Paper 75-54 presented at the AIAA 13th Aerospace Sciences Meeting held in Pasadena, Calif./January 20-22, 1975 containing three (3) somewhat discernible {standard format} programs for the HP-65; 1) Low thrust Inclination changes for circular base orbit, 2) Spacecraft mass at time t & 3) Inclination correction. I am somewhat reticent to post the complete paper considering the legibility of the hand written code.
[attachment=12378]

any takers to confirm the Program Documentation ?

BEST!
SlideRule

ps: cataract surgery restores much but not all.
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