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- 22:35, 4 September 2009 (diff | hist) . . (-14) . . Talk:Heat transfer coefficient (current)
- 22:34, 4 September 2009 (diff | hist) . . (+795) . . N Talk:Heat transfer coefficient (New page: Wikipedia gives some typical numbers for the heat transfer coefficients for air: Air - h = 10 to 100 W/(m2K) http://en.wikipedia.org/wiki/Heat_transfer_coefficient Since the martian atmo...)
- 11:57, 15 August 2009 (diff | hist) . . (-2) . . Tank geometries (→Sphere m)
- 11:56, 15 August 2009 (diff | hist) . . (+20) . . RocketDesignSpreadsheet (→Section 2 Oxidizer Tank Structure Mass) (current)
- 11:56, 15 August 2009 (diff | hist) . . (-1) . . RocketDesignSpreadsheet (→Sec-3 Fuel Tank Structure Mass)
- 11:50, 15 August 2009 (diff | hist) . . (+21) . . RocketDesignSpreadsheet (→Sec-3 Fuel Tank Structure Mass)
- 11:48, 15 August 2009 (diff | hist) . . (+61) . . RocketDesignSpreadsheet (→Section 2 Oxidizer Tank Structure Mass)
- 11:47, 15 August 2009 (diff | hist) . . (-2) . . Tank geometries (→Intro)
- 11:46, 15 August 2009 (diff | hist) . . (+1) . . Tank geometries (→(Surface Area)/(Volume^(2/3))
- 11:45, 15 August 2009 (diff | hist) . . (+4,144) . . N Tank geometries (New page: == Intro == As mentioned in RocketDesignSpreadsheet#Section_2_Oxidizer_Tank_Structure_Mass stated here, there are some important dimensionless quantities which determine how tanks scal...)
- 13:41, 14 August 2009 (diff | hist) . . (+1) . . SIL (→LOPA (Layers of Protection Analysis)
- 13:41, 14 August 2009 (diff | hist) . . (+611) . . SIL
- 13:35, 14 August 2009 (diff | hist) . . (+131) . . SIL (→Introduction)
- 13:34, 14 August 2009 (diff | hist) . . (-1) . . SIL (→Selection of SIL)
- 13:34, 14 August 2009 (diff | hist) . . (+4) . . SIL (→Sill Selection Matrices)
- 13:32, 14 August 2009 (diff | hist) . . (-24) . . SIL (→Risk Graphs)
- 13:31, 14 August 2009 (diff | hist) . . (+219) . . SIL (→Refferences)
- 13:31, 14 August 2009 (diff | hist) . . (+208) . . SIL (→Risk Graphs)
- 13:28, 14 August 2009 (diff | hist) . . (+25) . . SIL (→Risk Graphs)
- 13:28, 14 August 2009 (diff | hist) . . (+154) . . N File:Risk Graph.JPG (http://www.isa.org/Content/Microsites838/Safety_Division/Home818/ISA_2004_Safety_Papers/Different_SIL_Selection_Techniques_Can_Yield_Different_Answers.pdf) (current)
- 13:24, 14 August 2009 (diff | hist) . . (+1,182) . . SIL (→Sill Selection Matrices)
- 13:14, 14 August 2009 (diff | hist) . . (+324) . . N File:SILL Matrix.JPG (The above shows a 3D SILL Section matrix. The required reliability of a safety function is dependent both on the severity of an event and the likelihood of an event. http://www.isa.org/Content/Microsites838/Safety_Division/Home818/ISA_2004_Safety_Pape) (current)
- 13:07, 14 August 2009 (diff | hist) . . (+1,667) . . N SIL (New page: == Introduction == Safety Integrity Level (SIL) is defined as a relative level of risk-reduction provided by a safety function, or to specify a target level of risk reduction. In simple te...)
- 13:00, 14 August 2009 (diff | hist) . . (+221) . . N File:Fatality graph.JPG (http://4-sightconsulting.co.uk/Current_Papers/Determining_SILs/Methods_of_Determining_Safety_Integrity_Level.pdf The HSE have suggested that a risk of one 50 fatality event in 5,000 years is intolerable (HSE Books 2001).) (current)
- 23:55, 13 August 2009 (diff | hist) . . (+1) . . Optimal ground launch flight path (→A Visual Basic Function to Calculate the Optimal Flight Path) (current)
- 22:07, 13 August 2009 (diff | hist) . . (+8) . . Optimal ground launch flight path (→A Visual Basic Function to Calculate the Optimal Flight Path)
- 16:23, 13 August 2009 (diff | hist) . . (+64) . . Optimal ground launch flight path (→A Visual Basic Function to Caculate the Optimal Flight Path)
- 02:01, 13 August 2009 (diff | hist) . . (+539) . . Optimal ground launch flight path (→Total Gravity Losses)
- 01:59, 13 August 2009 (diff | hist) . . (+32) . . Optimal ground launch flight path (→Introduction)
- 01:57, 13 August 2009 (diff | hist) . . (+167) . . Optimal ground launch flight path
- 01:51, 13 August 2009 (diff | hist) . . (+2,766) . . N Optimal ground launch flight path (New page: The current derivation of the rocket equation on wikipedia (Aug 13 2009) seems to be overly cumbersome: http://en.wikipedia.org/wiki/Tsiolkovsky_rocket_equation Relay, it comes down to th...)
- 01:29, 13 August 2009 (diff | hist) . . (-3) . . RocketDesignSpreadsheet (→Sec 4 Rocket Performance)
- 01:15, 13 August 2009 (diff | hist) . . (+84) . . RocketDesignSpreadsheet (→Refferences)
- 01:15, 13 August 2009 (diff | hist) . . (+270) . . RocketDesignSpreadsheet (→Sec 4 Rocket Performance)
- 01:02, 13 August 2009 (diff | hist) . . (+161) . . RocketDesignSpreadsheet (→Refferences)
- 01:01, 13 August 2009 (diff | hist) . . (+430) . . RocketDesignSpreadsheet (→Sec 4 Rocket Performance)
- 00:48, 13 August 2009 (diff | hist) . . (+320) . . RocketDesignSpreadsheet (→Sec_3-Fuel-Tank-Structure-Mass)
- 00:47, 13 August 2009 (diff | hist) . . (0) . . RocketDesignSpreadsheet (→Section 2 Oxidizer Tank Structure Mass)
- 00:43, 13 August 2009 (diff | hist) . . (+1,709) . . RocketDesignSpreadsheet (→Section 2 Tank Structure Mass)
- 00:25, 13 August 2009 (diff | hist) . . (-1) . . RocketDesignSpreadsheet (→Section 1 Tank Volumes and Fuel Mass)
- 00:23, 13 August 2009 (diff | hist) . . (+790) . . RocketDesignSpreadsheet
- 00:11, 13 August 2009 (diff | hist) . . (+307) . . RocketDesignSpreadsheet
- 00:10, 13 August 2009 (diff | hist) . . (0) . . N File:RDS-Sec 4-Rocket-Performance.JPG (current)
- 00:08, 13 August 2009 (diff | hist) . . (0) . . N File:Sec 4 - Performance.JPG (current)
- 00:07, 13 August 2009 (diff | hist) . . (0) . . N File:Sec 3-Fuel-Tank-Structure-Mass.JPG (current)
- 00:04, 13 August 2009 (diff | hist) . . (0) . . N File:RDS-Sec 2-Oxidizer Tank Structure Mass.JPG (current)
- 23:59, 12 August 2009 (diff | hist) . . (0) . . N File:RDS-Sec1-Tank-Volumes-And-Fuel-Mass.JPG (current)
- 16:42, 9 August 2009 (diff | hist) . . (+1,195) . . RocketDesignSpreadsheet
- 22:50, 8 August 2009 (diff | hist) . . (+458) . . N Pressure Vessel (New page: == Wall Thickness == One requirement for the pressure vessel is for the walls to be strong enough to withstand the internal pressure. If you take a cross section of the pressure that is p...) (current)
- 21:46, 7 August 2009 (diff | hist) . . (+39) . . RocketDesignSpreadsheet
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