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Phase 2 Proposal Instructions for Cycle 10 | |||
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Tables and Figures
- Table4.1: Solar System Standard Targets
- Table4.2: Target Description Keywords
- Table4.3: Positional Parameters for TYPE = COMET
- Table4.4: Positional Parameters for TYPE = ASTEROID
- Table4.5: Parameters for TYPE = PGRAPHIC
- Table4.6: Parameters for TYPE = POS_ANGLE
- Table4.7: Parameters for TYPE = MAGNETO
- Table4.8: Parameters for TYPE = TORUS
- Table4.9: Parameters for TYPE = SAT
- Table4.10: Keywords for Observing Windows
- Table4.11: Operators for Observing Windows
- Table4.12: Formats for Specification of Target Flux Data
- Figure 4.1: Orbital Longitude for Satellites
- Figure 4.2: Orbital Longitude for Planets
HST is able to point at and track solar system targets with sub-arcsecond accuracy. In order for target acquisition and tracking to succeed, planetary observers must specify positions for their targets in a precise and unambiguous manner. Therefore, it is imperative that the Solar System Target List (SSTL) be carefully and correctly completed. This section explains how to fill out the SSTL for any solar system target.
Ephemerides are generated using fundamental ephemeris information from NASAÕs Jet Propulsion Laboratory (JPL). Ephemerides can be generated for all known types of solar system targets, including planets, satellites, comets, asteroids, surface features on planets and satellites, and offset positions with respect to the centers of all the above bodies. The following instructions demonstrate how to define solar system targets in a way that allows accurate ephemeris generation.
The body-axes definitions, body dimensions, directions of rotation poles, rotation rates, and the definitions of cartographic coordinates used by STScI are normally identical to the values adopted in the report of the ÒIAU Working Group on Cartographic Coordinates and Rotational Elements of the Planets and Satellites: 1982Ó (Davies, M.E., et al., Celestial Mechanics, 29, 309-321, 1983). In a few instances, the latter data have been updated due to new results obtained from the flyby spacecraft. Also, some new bodies have been added which were unknown at the time of the IAU report. For Jupiter and Saturn, the lambda(III) coordinate system is assumed, but lambda(I) or lambda(II) can be used. For Uranus and Neptune, coordinates follow the ÒReport of the IAU/IAG/COSPAR Working Group on Cartographic Coordinates and Rotation Rates of the Planets and SatellitesÓ (Celestial Mechanics and Dynamic Astronomy, 46, 197, 1989). If you need further information on these, please contact your Program Coordinator.
One exception exists to the requirements outlined above. Observers for solar system Targets of Opportunity (e.g. a ÒnewÓ comet or asteroid, a solar-wind disturbance reaching the Jovian magnetosphere, etc.), should complete the Generic Target List (See "Generic Targets List [Generic_Targets]" in Chapter 3.) and the Visit and Exposure Specifications (to the extent possible) in time for the Phase II deadline. If and when a suitable target appears, the proposer must complete the Solar System Target List and update the Visit and Exposure Specifications. No target can be observed until the complete Phase II information is provided.
In this chapter, each heading has a description followed by a keyword in square brackets (e.g., Target Number [Target_Number]). The keyword must be used in your RPS2 form. Elsewhere, items in boldface (e.g., RA-OFF) show words or phrases to be used directly as RPS2 entries. Items in brackets (e.g., <value>) show entries you are to provide. Parameters listed in square brackets (e.g., [A1 = <value>]) are optional, whereas those not in square brackets are required.
Space Telescope Science Institute http://www.stsci.edu Voice: (410) 338-1082 help@stsci.edu |
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