1989
DOI: 10.1029/ja094ia06p06866
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The plasma wake of the shuttle orbiter

Abstract: One of the objectives of the Plasma Diagnostics Package (PDP) instrumentation on Spacelab 2 was to obtain information about the plasma wake of the shuttle orbiter. We present plasma density and electron temperature data obtained (1) while the PDP was attached to the shuttle remote manipulator system and (2) while the PDP was a free‐flying satellite. Wake crossings by the PDP from ∼40 m to ∼240 m behind the orbiter provide information about the structure of the mid and far wake of the orbiter. As expected, the … Show more

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Cited by 32 publications
(16 citation statements)
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“…Figures a and b (top row) suggest that the electron density decreases as the spin‐phase angle approaches 180°, where the wake axis is expected to be directed. This density structure is commonly observed around a moving vehicle [e.g., Murphy et al ., ]. The wake effect obtained with the NEI also appears in the measurement data of the FLP as periodic changes in V‐I characteristics in synchronization with the spin period.…”
Section: Nei/pwm Observation and Analysis Resultsmentioning
confidence: 89%
“…Figures a and b (top row) suggest that the electron density decreases as the spin‐phase angle approaches 180°, where the wake axis is expected to be directed. This density structure is commonly observed around a moving vehicle [e.g., Murphy et al ., ]. The wake effect obtained with the NEI also appears in the measurement data of the FLP as periodic changes in V‐I characteristics in synchronization with the spin period.…”
Section: Nei/pwm Observation and Analysis Resultsmentioning
confidence: 89%
“…14 ' 15 The PDF was operated both on the RMS and in a free-flight path specifically designed to provide information on the characteristics of the wake both in the near vicinity of the Orbiter (within a body radius of the obstacle of about 10 m) and in the distant wake, out to about 250 m. From RMS and back-away observations, the density in the near wake can be two or more orders of magnitude less than the ambient density, whereas the electron temperature on the boundary of the wake region can be observed to increase by more than a factor of 2. At greater distances, the magnitude of the density depletion is less, sometimes only about 10%.…”
Section: Wake Studiesmentioning
confidence: 97%
“…A dielectric coating was applied to one side of the plate made of aluminum (length l = 45 cm, width 2R = 16 cm, and thickness δ ≈ 0.1 cm). An aluminum coating was applied (sprayed) onto the surface of the disk (made of quartz) 15 [4] for Sei ≈ 8, R ds ≈ 40, and −Φw ≈ 0 (5) and 20 (6); points 7-9 are the results measured in [12] in the ionosphere on the Explorer-C (AE-C) artificial satellite for 5.9 Sei 8.04, −Φw ≈ 10, and R ds ≈ 116.3 (7), 135.7 (8), and 162.5 (9); points 10 are the results measured in [13] in the ionosphere on the S3-2 artificial satellite for Sei ≈ 8, R ds 45, and −Φw ≈ 10; points 11 are the results measured in [14] in the wake behind the Space Shuttle for Sei ≈ 3.35 and R ds 2 · 10 3 ; (b) angular distribution of ion density nis(θ) at t = 0.192: points 1 are the results measured in [12] on the Explorer-C (AE-C) artificial satellite for Sei ≈ 7.83, R ds ≈ 73.4, −Φw ≈ 8.8, and ξei = 1.14; points 2 are the results measured in the present work (wake behind a cylinder for Sei ≈ 5.1, R ds ≈ 78, −Φw ≈ 6.7, and ξei = 4); curve 3 is the solution of Eq. (7) with the dependence nis(Φ) from [6] for Sei ≈ 5.1, R ds ≈ 80, and −Φw ≈ 6.7; points 4 are the results of the discrete flow model [11].…”
Section: High-voltage Charging Of the Leeward Surfaces Of A Solid By mentioning
confidence: 99%