SEE PRODUCTS / SEE Related Model & DB -
Ionizing
Radiation Environment
ORBITAL PARTICULATE TRAJECTORY
MODEL (OPT)
Description:
The Orbital
Particulate Trajectory Model (OPT) was constructed around the
JPL orbital trajectory program, Artificial Satellite Analysis
Program (ASAP). OPT was developed to provide a means of
predicting the motion of released particulates as a function
of time relative to the spacecraft coordinate system as well
as in an Earth centered coordinate system. OPT is useful in
determining particulate recontact potential based on
particulate release conditions, and for determining the
location of particulates in instrument fields-of-view as a
function of time.
Additional
Information:
Language: FORTRAN
Operating System:
UNIX
Hardware
Requirements: 100 Kbytes disk space, compiled executable
requires 0.5 MB total memory is less than 2MB for output
files.Availability:
- Maintenance/
Upgrades: No
- Source Code:
Yes
- Cost: $3000
- Distribution:
1/4 inch tape
- Manuals: Yes
- Training: Yes
Input Description:
Particulate characteristics, # of particulates, particulate
sizes.
Output Format:
FORTRAN Files- Tabular
Verification/
Validation: Based on JPL orbital mechanics code (ASAP)
Point of Contact:
Dr. Ray Rantanen
ROR Enterprises
Athol, ID 83801
Phone: 208-623-6376
Tim Gordon
Applied Science Technologies
Littleton, CO 80162
Phone: 303-973-7708
E-mail:
timgordon@aol.com
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