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The Ascent Roadmap

Saturday, December 20, 2008. Hypothetical Oxyhydrogen Propulsion Systems. Oxyhydrogen will never be practical in lower stages because it produces a lower total thrust pressure than other propellant combinations, including oxykerosene, which is currently the cheapest one. Sowhat would the Ascent Roadmap ever do with oxyhydrogen? In order to consider it, we must look at the sources of expense in existing oxyhydrogen engines and seek to eliminate or reduce them. Ones that can be helped:. There is some bad n...

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The Ascent Roadmap | ascentroadmap.blogspot.com Reviews

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Saturday, December 20, 2008. Hypothetical Oxyhydrogen Propulsion Systems. Oxyhydrogen will never be practical in lower stages because it produces a lower total thrust pressure than other propellant combinations, including oxykerosene, which is currently the cheapest one. Sowhat would the Ascent Roadmap ever do with oxyhydrogen? In order to consider it, we must look at the sources of expense in existing oxyhydrogen engines and seek to eliminate or reduce them. Ones that can be helped:. There is some bad n...

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1 the ascent roadmap

2 posted by

3 terry wilson

4 no comments

5 prochron heads up

6 prochron spreadsheet

7 key=ppw38bhxyutk3x dmy2jfoa

8 prochron update

9 terry

10 accomplishments

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The Ascent Roadmap | ascentroadmap.blogspot.com Reviews

https://ascentroadmap.blogspot.com

Saturday, December 20, 2008. Hypothetical Oxyhydrogen Propulsion Systems. Oxyhydrogen will never be practical in lower stages because it produces a lower total thrust pressure than other propellant combinations, including oxykerosene, which is currently the cheapest one. Sowhat would the Ascent Roadmap ever do with oxyhydrogen? In order to consider it, we must look at the sources of expense in existing oxyhydrogen engines and seek to eliminate or reduce them. Ones that can be helped:. There is some bad n...

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ascentroadmap.blogspot.com

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The Ascent Roadmap: November 2008

http://ascentroadmap.blogspot.com/2008_11_01_archive.html

Friday, November 28, 2008. 1st digit: number of modules in Stage Two. 2nd digit: number of modules in Stage Three. 3rd and 4th digits: 10kg units of Stage Four. Version 1000: The sounding rocket (has 4 modules in Stage One). Total impulse is 445860Ns, lower S class and about half of the maximum allowable under FAA amateur rocketry rules. It has to carry a payload of at least 100kg in order to stay under the amateur ceiling. Version 4104: Payload of 5kg, Gross mass is 890.2kg, has 12 Stage One motors.

2

The Ascent Roadmap: Prochron 0811B

http://ascentroadmap.blogspot.com/2008/11/prochron-0811b.html

Saturday, November 22, 2008. It's official: Prochron 0811B specs. Booster on pad: RTL fuelled: 695kg. Booster on pad: RTL unfuelled: 141kg (Stage One installed). Booster on truck: not fuelled: 75kg (Stage One not installed). Stage One: Cesaroni M4770-P http:/ www.pro38.com/motor/M4770-P.html. 66kg total per module; ten modules. Stage Two: Prochron module * 3. Stage Three: Prochron module *1. Stage Four: Prochron upper stage. Fairing: 4kg, payload 5kg (i.e.: 3kg Cubesat plus 2kg deployer). 2 Module burn t...

3

The Ascent Roadmap: Prochron Spreadsheet

http://ascentroadmap.blogspot.com/2008/12/prochron-spreadsheet.html

Saturday, December 6, 2008. I've decided to post online the basic optimization spreadsheet at:. Http:/ spreadsheets.google.com/pub? The grey ones are not optimal. Subscribe to: Post Comments (Atom). Hypothetical Oxyhydrogen Propulsion Systems. Ascent Roadmap Propellant Decisions. View my complete profile.

4

The Ascent Roadmap: Prochron Update

http://ascentroadmap.blogspot.com/2008/11/prochron-update.html

Friday, November 28, 2008. 1st digit: number of modules in Stage Two. 2nd digit: number of modules in Stage Three. 3rd and 4th digits: 10kg units of Stage Four. Version 1000: The sounding rocket (has 4 modules in Stage One). Total impulse is 445860Ns, lower S class and about half of the maximum allowable under FAA amateur rocketry rules. It has to carry a payload of at least 100kg in order to stay under the amateur ceiling. Version 4104: Payload of 5kg, Gross mass is 890.2kg, has 12 Stage One motors.

5

The Ascent Roadmap: Prochron Heads Up

http://ascentroadmap.blogspot.com/2008/12/prochron-heads-up.html

Tuesday, December 16, 2008. There is some bad news for Prochron.the Isp's used in the spreadsheet and previous posts are too high for the first stage. I saw this when I dug up my April 2007 notes for Symtex. The new Isps are about 2100m/s at sea level, 2700m/s in vacuum, but it should still be possible to achieve 3000m/s in the upper stages and on the OpenLuna lander versions. Subscribe to: Post Comments (Atom). Hypothetical Oxyhydrogen Propulsion Systems. Ascent Roadmap Propellant Decisions.

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After Columbia STS-107

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Scobee, Smith, Onizuka, Resnik, McNair, Jarvis, McAuliffe (28 January 1986). Husband, McCool, Clark, Chalwa, Ramon, Anderson, Brown (1 February 2003). Homer the Cat (21 June 2007). Welcome to After Columbia. On 1 February 2009 (happened to be the sixth anniversary of. Unfortunate end), Terry Wilson, the only active member of After Columbia at the time, received a waking vision launching his new project,. Sprint Program, Mars Challenger, Ascent Roadmap. After Columbia Mars Direction,. This mission uses ti...

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The Ascent Roadmap

Saturday, December 20, 2008. Hypothetical Oxyhydrogen Propulsion Systems. Oxyhydrogen will never be practical in lower stages because it produces a lower total thrust pressure than other propellant combinations, including oxykerosene, which is currently the cheapest one. Sowhat would the Ascent Roadmap ever do with oxyhydrogen? In order to consider it, we must look at the sources of expense in existing oxyhydrogen engines and seek to eliminate or reduce them. Ones that can be helped:. There is some bad n...

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