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pro vyhledávání: '"Wallace T. Fowler"'
Autor:
Wallace T. Fowler, Carrie D. Olsen
Publikováno v:
The Journal of the Astronautical Sciences. 55:293-309
This paper examines final rendezvous between two vehicles in highly elliptic orbits. The range of eccentricities addressed is 0.6 to 0.9. Due to the varying orbital speeds of the two vehicles, the relative motion during elliptic rendezvous is highly
Autor:
Payam Banazadeh, Chinmay Aladangady, Wallace T. Fowler, Joseph Lazio, Daniel P. Scharf, Dayton L. Jones
Publikováno v:
2013 IEEE Aerospace Conference.
Seeking “nearby habitable worlds” was one of three science themes identified in the Astronomy Decadal Survey. Hundreds of extrasolar planets are known, but magnetic fields are likely required for these planets to be habitable. As of today, no dir
Publikováno v:
Acta Astronautica. 35:445-454
Due to Mercury's small mass and position deep within the solar gravitational well, an orbiter mission poses difficult performance requirements (i.e. ΔV, thermal extremes). However, Yen (JPL) showed that with extended trip times, substantial Mercury
Autor:
Chirag B. Patel, Kaitlin E. Gushwa, Jaime I. Cervantes, Ana Guerrero de la Peña, Wallace T. Fowler
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
The icy Jovian moon Europa is considered a top priority target by the scientific community because it appears to have the conditions necessary to harbor life. Deployable Orbiter Rover Reconnaissance Assembly (DORRA) the Europa Explorer is a conceptua
Publikováno v:
Journal of Spacecraft and Rockets. 30:420-425
Many current manned Mars mission studies are using low lift-to-drag ratio vehicles to aerobrake at both Mars and Earth. This paper will demonstrate that if entry velocity constraints are incorporated into the interplanetary analysis of aerobraking Ma
Publikováno v:
Journal of Spacecraft and Rockets. 30:426-430
Many current manned Mars mission studies are using low lift-to-drag ratio (L/D) vehicles to aerobrake at both Mars and Earth. The use of these low L/D vehicles could limit the allowable velocity at the atmospheric interface. This paper will demonstra
Publikováno v:
Journal of Spacecraft and Rockets. 38:289-291
Autor:
Wallace T. Fowler
Publikováno v:
Eshbach's Handbook of Engineering Fundamentals, Fifth Edition
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::77b10b33896e949ba74904e77798db15
https://doi.org/10.1002/9780470432754.ch3
https://doi.org/10.1002/9780470432754.ch3
Autor:
Wallace T. Fowler, Lisa Guerra
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Publikováno v:
SPIE Proceedings.
There has been a recent increase in emphasis on small satellites because of their low cost, short development times, relative simplicity, and cost efficiency. However, these satellites do have drawbacks. Their small size results in small surface area