SPEAR 3 flight analysis: Grounding by neutral gas release, and magnetic field effects on current distribution

The Space Power Experiment Aboard Rockets (SPEAR) 3 experiment was launched on March 15, 1993, to test grounding devices for negative payloads. In this paper we review two aspects of the high-altitude flight data and compare them with preflight predictions. The SPEAR 3 neutral gas release experiment studied a grounding mechanism observed on previous flights during attitude control system (ACS) firings. Preflight calculations using Paschen law physics generalized to three dimensions predicted that the high rate gas release (about one order of magnitude below normal ACS) would reduce the rocket potential to within 200–300 V of plasma ground. The flight data is well fit by a value of −225 V. Orientation relative to Earth's magnetic field had no effect on the floating potential or grounding operations but had a large effect on the portion of the current collected by the boom. We compare these flight measurements with preflight calculations made with the DynaPAC computer code.

[1]  Susumu Sasaki,et al.  VLF Wave Experiments in Space Using a Modulated Electron Beam , 1995 .

[2]  N. B. Myers,et al.  Recent observations of high voltage spacecraft-environment interaction at LEO altitudes using sounding rockets , 1990 .

[3]  M. Mandell,et al.  Sheath physics and potential mitigation on the SPEAR-III rocket experiment , 1994 .

[4]  N. B. Myers,et al.  Computer modeling of current collection by the CHARGE-2 mother payload , 1990 .

[5]  Ira Katz,et al.  TSS‐1R electron currents: Magnetic limited collection from a heated presheath , 1998 .

[6]  N. B. Myers,et al.  A comparison of current-voltage relationships of collectors in the earth's ionosphere with and without electron beam emission , 1989 .

[7]  Phelps,et al.  Excitation of N2 in dc electrical discharges at very high E/n. , 1987, Physical review. A, General physics.

[8]  P. Rodriguez,et al.  A method for measuring large changes in the payload voltage of rockets and satellites , 1995 .

[9]  Susumu Sasaki,et al.  Electron collection enhancement arising from neutral gas jets on a charged vehicle in the ionosphere , 1990 .

[10]  R. A. Kuharski,et al.  Structure of the bipolar plasma sheath generated by SPEAR I , 1989 .

[11]  I. Katz,et al.  Electrical Breakdown Currents on Large Spacecraft in Low Earth Orbit , 1994 .

[12]  D. Morgan,et al.  Payload environment and gas release effects on sounding rocket neutral pressure measurements , 1996 .

[13]  R. A. Kuharski A quick accurate model of nozzle backflow , 1991 .