Spin rate of galileo probe during descent into the atmosphere of jupiter

Journal of Spacecraft and Rockets

Volumn 35, Issue 1, 1998, Pages 100-102

  Lanzerotti, L J ^a,f   Rinnert, K ^b   Carlock, D ^c,g,h   Sobeck, C K ^d,i   Dehmel, G ^e,j  

^a LUCENT TECHNOLOGIES   (United States)

^b MAX PLANCK INSTITUT FÜR SONNENSYSTEMFORSCHUNG   (Germany)

^c BOEING COMPANY   (United States)

^d NASA AMES RESEARCH CENTER   (United States)

^e TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

^f Technical Staff   (United States)

^g Spacecraft Engineering Operations ^*

^h AIAA   (United States)

ⁱ Space Projects Division ^*

^j Institut für Nachrichtentechnik

more..

Author keywords

[No Author keywords available]

Indexed keywords

DETECTORS; EQUATIONS OF MOTION; EXTRATERRESTRIAL ATMOSPHERES; MAGNETOSPHERE; PLANETS; TRAJECTORIES;

DESCENT MODULE; GALILEO PROBE; JUPITER; SPIN RATE;

SPACE PROBES;

EID: 0031704166     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/3.27003     Document Type: Article

References (9)

1. Lanzerotti, L. J., Rinnert, K., Dehmel, G., Gliem, F. O., Krider, E. P., Uman, M. A., Umlauft, G., and Bach, J., "The Lightning and Radio Emission Detector (LRD) Instrument," Space Science Reviews, Vol. 60, Nos. 1-4, 1992, pp. 91-109.
2. Oswald, T. W., "Spin Vane Angles for Descent Module," Missile Systems Group, Hughes Aircraft Co., Hughes IDC HS373-3131, Canoga Park, CA, Aug. 1983.
3. "Probe System and Related Requirements," Galileo Probe Project, NASA Ames Research Center, ARC Specification JP 510.00 (Rev. 4), Moffett Field, CA, Feb. 1982.
4. Oswald, T. W., "Galileo Probe Descent Module Aerodynamics Final Report," Missile Systems Group, Hughes Aircraft Co., Hughes IDC HS373-3190, Canoga Park, CA, Oct. 1983.
5. Rubin, L., "Spin Vane Angle Tolerance," Missile Systems Group, Hughes Aircraft Co., Hughes IDC HS373-4335, El Segundo, CA, Nov. 1988.
6. Kim, V., "Spin Vane Angle Verification," Space and Communications Group, Hughes Aircraft Co., Hughes TSS V095, El Segundo, CA, April 1989.
7. Radecki, J. T., "Pre Ship Viewgraph Book: Descent Module Aerodynamics," Space and Communications Group, Hughes Aircraft Co., Hughes IDC HS373-3297, El Segundo, CA, Feb. 1984.
8. Talley, R. G., "Galileo Probe Deceleration Module Final Report," ReEntry Systems Operations, General Electric Co., Document 84SDS2020, Philadelphia, PA, Jan. 1984.
9. Neff, J. M. (ed.), "Galileo Probe-Orbiter Relay Link Integration Report: Figure 4.3-6, Phase Error Contributions to PLL Due to Environmental Effects," JPL D-1038(C)/NASA 1625-145(C), Pasadena, CA, Oct. 1994.