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Important Announcement: Application Deadline Extended
New Editor-in-Chief Sought for the Journal of Propulsion and Power
Vigor Yang, current Editor-in-Chief of the Journal of Propulsion and Power, will step down from his position after 8 years of service at the end of 2009. We are seeking an outstanding candidate with an international reputation for this position, and we invite your nominations. This is an open process, and the final selection will be made only on the basis of the applicants’ merits.

The Journal of Propulsion and Power was founded in the early 1980s to promote the advancement in airbreathing, electric, and advanced propulsion, solid and liquid rockets, combustion, fuels and propellants, power generation and conversion for aerospace vehicles, and terrestrial energy devices and systems. While the original concept for the journal originated from AIAA’s Airbreathing Propulsion TC, the early exploration of the concept broadened the journal’s scope to encompass rocket technologies and basic combustion phenomena related to propulsion. Furthermore because the decision had been made to suspend publication of AIAA’s Journal of Energy, energy conversion papers were also included in the scope.

Today aerospace propulsion and power remain critical technical issues as we look for new sources of power for space exploration as well as more efficient and environmentally responsible power sources for terrestrial applications in general and aerospace vehicles in particular. JPP will be critical as the journal of record for this research. The next editor-in-chief will play a critical role in documenting the discoveries and advances to come.

The Editor-in-Chief is responsible for maintaining the quality and reputation of the journal. He or she receives manuscripts, assigns them to Associate Editors for review and evaluation, and monitors the performance of the Associate Editors to ensure that the manuscripts are processed in a fair and timely manner. The Editor-in-Chief works closely with AIAA Headquarters staff on both general procedures and the scheduling of specific issues. Detailed record keeping and prompt actions are required. The Editor-in-Chief is expected to provide his or her own clerical support, although this may be partially offset by a small expense allowance. AIAA provides a computer and a Web-based manuscript-tracking system.

Interested candidates are invited to send full résumés, including a complete list of published papers, to:

Rodger Williams
American Institute of Aeronautics and Astronautics
1801 Alexander Bell Drive, Suite 500
Reston, VA 20191-4344
Fax: 703.264.7551
E-mail: rodgerw@aiaa.org

Two letters of recommendation also are required. The recommendations should be sent by the parties writing the letters directly to Mr. Williams at the above address, fax number, or e-mail. All materials must be received at AIAA Headquarters by 30 June 2009.

A selection committee will review the applications and will recommend qualified candidates to the AIAA Vice President–Publications, who in turn will present a recommendation to the AIAA Board of Directors for approval. All candidates will be notified of the final decision.

JOURNAL OF SPACECRAFT AND ROCKETS
Editor-in-Chief :
E. Vincent Zoby

NASA Langley Research Center
Frequency Bimonthly
ISSN 0022-4650
E-ISSN 1533-6794
CURRENT ISSUE
2009 vol. 46 no. 3

Influence of Ablation on Radiative Heating for Earth Entry
pages (481-491)
doi: 10.2514/1.40290
    Christopher O. Johnston; Peter A. Gnoffo; Kenneth Sutton
Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles
pages (492-500)
doi: 10.2514/1.40197
    Daniele Bianchi; Francesco Nasuti; Emanuele Martelli
Comparison of Materials for an Integrated Thermal Protection System for Spacecraft Reentry
pages (501-513)
doi: 10.2514/1.35669
    Christian Gogu; Satish K. Bapanapalli; Raphael T. Haftka; Bhavani V. Sankar
Effective Thermal/Mechanical Properties of Honeycomb Core Panels for Hot Structure Applications
pages (514-525)
doi: 10.2514/1.30408
    Javad Fatemi; Martin Lemmen
Kinetics and Thermophysical Properties of Polymer Nanocomposites for Solid Rocket Motor Insulation
pages (526-544)
doi: 10.2514/1.39798
    D.W. K. Ho; Joseph H. Koo; Ofodike Ezekoye
Supersonic/Hypersonic Laminar Heating Correlations for Rectangular and Impact-Induced Open and Closed Cavities
pages (545-560)
doi: 10.2514/1.36830
    Joel L. Everhart
Effect of a Rearward-Facing Step on Plasma Ignition in Supersonic Flow
pages (561-567)
doi: 10.2514/1.39018
    Junya Watanabe; Naoyuki Abe; Kenichi Takita
Numerical Study of Plasma-Assisted Aerodynamic Control for Hypersonic Vehicles
pages (568-576)
doi: 10.2514/1.39032
    Nicholas J. Bisek; Iain D. Boyd; Jonathan Poggie
Investigation of Missile-Shaped Body with Forward-Facing Cavity at Mach 8
pages (577-591)
doi: 10.2514/1.38914
    Saravanan Selvaraj; Jagadeesh Gopalan; K.P.J. Reddy
Optimal Aft End Distorted Fin Model Using Response Surface Method
pages (592-598)
doi: 10.2514/1.40496
    Se-Yoon Oh; Seung O. Park
Ground Effects for Widely Spaced, Supersonic, Vertical Retrorockets
pages (599-605)
doi: 10.2514/1.36299
    Richard E. Wirz; Shaun S. Shariff
Flare-Type Membrane Aeroshell Flight Test at Free Drop from a Balloon
pages (606-614)
doi: 10.2514/1.40912
    Kazuhiko Yamada; Daisuke Akita; Eiji Sato; Kojiro Suzuki; Tomohiro Narumi; Takashi Abe
PRISMA: An In-Orbit Test Bed for Guidance, Navigation, and Control Experiments
pages (615-623)
doi: 10.2514/1.40161
    Per Bodin; Robin Larsson; Fredrik Nilsson; Camille Chasset; Ron Noteborn; Matti Nylund
Demonstration of a Wire Suspension for Wind-Tunnel Virtual Flight Testing
pages (624-633)
doi: 10.2514/1.39188
    John C. Magill; Paolo Cataldi; Joseph R. Morency; Daniel X. Hammer; Riley Burgess; Edward Jeter
Science Operations Planning Optimization for Spacecraft Formation Flying Maneuvers
pages (634-644)
doi: 10.2514/1.40490
    Ross Burgon; Peter Roberts; Jennifer Roberts; Finn Ankersen
Asteroid Diversion Using Long Tether and Ballast
pages (645-661)
doi: 10.2514/1.40828
    David B. French; Andre P. Mazzoleni
Effects of Self-Shadowing on Nonconservative Force Modeling for Mars-Orbiting Spacecraft
pages (662-669)
doi: 10.2514/1.41679
    Erwan Mazarico; Maria T. Zuber; Frank G. Lemoine; David E. Smith
Solar Sail Formation Flying for Deep-Space Remote Sensing
pages (670-678)
doi: 10.2514/1.42404
    James Douglas Biggs; Colin McInnes
Analysis of Space Shuttle Primary Reaction-Control Engine-Exhaust Transients
pages (679-688)
doi: 10.2514/1.39516
    Benjamin D. Hester; Yu-Hui Chiu; Jeremy R. Winick; Rainer A. Dressler; Lawrence S. Bernstein; Matthew Braunstein; Paul F. Sydney
Influence of Power Supplies on the Secondary Arc Test of Solar Arrays
pages (689-696)
doi: 10.2514/1.40942
    Teppei Okumura; Kazuhiro Toyoda; Mengu Cho; Andreas Kroier; Erich Leitgeb
Environmental Effects on Solar Array Electrostatic Discharge Current Waveforms and Test Results
pages (697-705)
doi: 10.2514/1.41696
    Teppei Okumura; Hirokazu Masui; Kazuhiro Toyoda; Mengu Cho; Kumi Nitta; Mitsuru Imaizumi
Measurement Interpolation Methods for Dual One-Way Ranging Systems
pages (706-711)
doi: 10.2514/1.42261
    Jeongrae Kim; Young Jae Lee
New Radiation Dose Model for Geostationary Orbit
pages (712-715)
doi: 10.2514/1.40996
    Ravinarayana Bhat
Mitigation Method of Spacecraft Momentum by Solar Radiation Pressure
pages (716-719)
doi: 10.2514/1.37505
    Seongkyun Jeong; Sanguk Lee; Hae-Yeon Kim; Jae-Hoon Kim
Stationkeeping of Geosynchronous Spacecraft Using a Hybrid Orbit Propagator and Optimization Technique
pages (719-724)
doi: 10.2514/1.40784
    Tae Soo No; Okchul Jung; S.-C. Lee
Genetic Design of Target Orbits for a Temporary Reconnaissance Mission
pages (725-728)
doi: 10.2514/1.41620
    Hae-Dong Kim; Hyochoong Bang; Ok-Chul Jung
Photometric Detection of Known Sun-Occluding Satellites
pages (728-733)
doi: 10.2514/1.41593
    Brian Poller; Robert D. Culp
Aerospace Materials Property Database (TPSX)
pages (733-736)
doi: 10.2514/1.43777
    Thomas H. Squire; Frank S. Milos; George C. Hartlieb
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The American Institute of Aeronautics and Astronautics (AIAA) is the world's largest technical society dedicated to the global aerospace profession.