Farquhar et al., 1976 - Google Patents
Mission design for a halo orbiter of the EarthFarquhar et al., 1976
- Document ID
- 12009595053679220924
- Author
- Farquhar R
- Muhonen D
- Richardson D
- Publication year
- Publication venue
- Astrodynamics Conference
External Links
Snippet
In 1978, a scientific satellite will be stitioned in the vicinity of the sun-earth intcrior libration point. At this location, it will he able to continuously monitor the interplanetary medium between the sun and the earth. Data rates can be maintained at high levels because the …
- 125000001475 halogen functional group 0 title abstract description 34
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- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/281—Spin-stabilised spacecraft
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- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/58—Thermal protection, e.g. heat shields
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