urn:nasa:pds:dawn-grand-vesta:browse
1.0
DAWN GRaND Vesta Bundle: Browse Collection
1.11.0.0
Product_Collection
Prettyman, T.H.; Yamashita, N.
2021
Browse files for the GRaND Vesta bundle.
2021-01-06
1.0
Initial Revision
DAWN Mission to Vesta and Ceres
Mission
urn:nasa:pds:context:investigation:mission.dawn_mission_to_vesta_and_ceres
collection_to_investigation
DAWN
Spacecraft
The Dawn spacecraft is an ion-propelled spacecraft capable of visiting and stopping at multiple targets in the Main Asteroid Belt. Most of the spacecraft design was provided by Orbital Sciences Corporation (Orbital), and the Jet Propulsion Laboratory (JPL) provided the ion propulsion system (IPS) and parts of the electrical power system and telecommunications system. Orbital was responsible for overall assembly, including integration of instruments, system-level tests, and launch operations. JPL is responsible for mission operations. The IPS is an expanded version of the system operated extensively on Deep Space 1 (DS1). The spacecraft design benefits from inheritance from previous projects at Orbital and the JPL. The mechanical design is based on Orbital's Star-2 series, and the avionics draw from the LEOStar-2 series. There is significant redundancy throughout the design, and the mission can be accomplished in the presence of most credible single faults. A complete description of the Dawn spacecraft may be found in Rayman et al. (2006), from which most of the information in this file was taken.
urn:nasa:pds:context:instrument_host:spacecraft.dawn
is_instrument_host
GAMMA-RAY AND NEUTRON DETECTOR for DAWN
Instrument
urn:nasa:pds:context:instrument:dawn.grand
is_instrument
(4) Vesta
Asteroid
urn:nasa:pds:context:target:asteroid.4_vesta
bundle_to_target
Browse
collection_inventory_browse.csv
0
PDS DSV 1
79
Carriage-Return Line-Feed
Comma
2
0
Member Status
1
ASCII_String
1
%1s
LIDVID_LID
2
ASCII_LIDVID_LID
255
%-255s
inventory_has_member_product