Early Application of Solar-electric Propulsion to a 1-astronomical-unit Out-of-the-ecliptic Mission PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Early Application of Solar-electric Propulsion to a 1-astronomical-unit Out-of-the-ecliptic Mission PDF full book. Access full book title Early Application of Solar-electric Propulsion to a 1-astronomical-unit Out-of-the-ecliptic Mission by William C. Strack. Download full books in PDF and EPUB format.
Author: William C. Strack
Publisher:
ISBN:
Category : Electric propulsion
Languages : en
Pages : 28
Get Book Here
Book Description
Current technology for solar-electric propulsion is used to assess the potential performance advantages of low-thrust propulsion for an out-of-the-ecliptic mission. Simple normal-to-the-orbit thrust steering is assumed with coast subarcs permitted. The electric spacecraft is launched onto an Earth escape trajectory by an Atlas (SLV3C)-Centaur or a Titan IIIC. Comparisons with a similarly launched uprated Burner II stage reveal that significant performance gains are possible using the electric stage with 250- to 475-day flight times.
Author: William C. Strack
Publisher:
ISBN:
Category : Electric propulsion
Languages : en
Pages : 28
Get Book Here
Book Description
Current technology for solar-electric propulsion is used to assess the potential performance advantages of low-thrust propulsion for an out-of-the-ecliptic mission. Simple normal-to-the-orbit thrust steering is assumed with coast subarcs permitted. The electric spacecraft is launched onto an Earth escape trajectory by an Atlas (SLV3C)-Centaur or a Titan IIIC. Comparisons with a similarly launched uprated Burner II stage reveal that significant performance gains are possible using the electric stage with 250- to 475-day flight times.
Author: William C. Strack
Publisher:
ISBN:
Category : Electric propulsion
Languages : en
Pages : 21
Get Book Here
Book Description
Current technology for solar-electric propulsion is used to assess the potential performance advantages of low-thrust propulsion for an out-of-the-ecliptic mission. Simple normal-to-the-orbit thrust steering is assumed with coast subarcs permitted. The electric spacecraft is launched onto an Earth escape trajectory by an Atlas (SLV3C)-Centaur or a Titan IIIC. Comparisons with a similarly launched uprated Burner II stage reveal that significant performance gains are possible using the electric stage with 250- to 475-day flight times.
Author: William C. Strack
Publisher:
ISBN:
Category :
Languages : en
Pages : 21
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 412
Get Book Here
Book Description
Author: William C. Strack
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1162
Get Book Here
Book Description
Author: Frank J. Hrach
Publisher:
ISBN:
Category : Interplanetary voyages
Languages : en
Pages : 44
Get Book Here
Book Description
Author: Robert Duncan Enzmann
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 886
Get Book Here
Book Description
Author: Thomas Lincoln Casey
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 476
Get Book Here
Book Description
Records of meetings 1808-1916 in v. 11-27.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Get Book Here
Book Description
