PeZook wrote:Well, mine gave me a failure in Selene 6, which means another LM test flight is inevitable. That means Selene 7 in Q4 2016, and Selene 8 in Q1 2017, with the landing on Selene 9.
Unless we accept the risk an upgrade 7 to a lunar orbital test...
And then we can have a LITERAL race to the Moon! IN SPACE!
A question, though: does the MSA release their launch scheules publically? If you don't it's no biggie, we'll just have Lev steal them, but I have to ask
EDIT: BTW, one of these days I'm totally gonna have to put together a novaterran Moon mission in Orbiter
I know this is dragging up from the past but since I've got all my files back together I'm finally getting around to posting everything. This will include, in about another 30 minutes the flight list through Daedalus 8 which is also, probably in an hour or so, going to go up into the Wiki. If you've got questions about the material below let me know because here is how I've been rolling things:
I do everything in Excel with an =RANDBETWEEN(1,100) for each launch and in the case of actual landings the descent phase. For the missions with 2 units (Pegasus 8,9, and 10 and all Daedalus missions starting with 3) the second rocket is indicated as -B and when there are landings/practice landings it is indicated by -C.
The success percentages are:
Result
Total Success, All Systems
Success, 1-2 Minor Failures
Partial Success, one major or multiple minor failures
Partial Failure, multiple major system failure, degenerative orbit reached
Total Failure, destroyed on launch pad
Abbreviation
TS
S
PS
PF
TF
As each mission series gets entered I physically re-type the current =RAND so that it doesn't keep switching around on me and this is currently complete through the end of the Daedalus program in 2018. Note that I've added 2 additional moon shots which may or may not get cancelled depending upon whether or not we can get the "Eagle" spaceborne. Those 2 extra shots are basically being paid for with a combination of an extra bit of Canisian money and the funds made available by Cascadia for putting one of their astronauts on Daedauls 5,6,7,10, and 13. Though I should add that I've only done full crew rosters through Daedalus 8 and that is all that will be released.
Mission results data:
Value
88
65
67
72
87
76
57
68
35
86
74
37
41
98
53
76
74
78
100
65
34
71
79
98
67
55
28
98
39
71
31
7
N/A
N/A
79
30
64
100
2
N/A
30
26
37
97
16
18
64
35
93
57
35
Result
TS
S
S
S
TS
S
S
S
S
TS
S
S
S
TS
S
S
S
S
TS
S
S
S
S
TS
S
S
S
TS
S
S
S
PS
N/A
N/A
S
S
S
TS
TF
N/A
S
S
S
TS
S
S
S
S
TS
S
S
Mission
Peg1
Peg2
Peg3
Peg4
Peg5
Peg6
Peg7
Peg8
Peg8-B
Peg9
Peg9-B
Peg10
Peg10-B
Daed1
Daed2
Daed3
Daed3-B
Daed4
Daed4-B
Daed5
Daed5-B
Daed5-C
Daed6
Daed6-B
Daed6-C
Daed7
Daed7-B
Daed7-C
Daed8
Daed8-B
Daed8-C
Daed9
Daed9-B
Daed9-C
Daed10
Daed10-B
Daed10-C
Daed11
Daed11-B
Daed11-C
Daed12
Daed12-B
Daed12-C
Daed13
Daed13-B
Daed13-C
Daed13-D
Daed14
Daed14-B
Daed14-C
Daed14-D
Date
Q2 2014
Q3 2014
Q3 2014
Q4 2014
Q4 2014
Q1 2015
Q2 2015
Q3 2015
Q3 2015
Q4 2015
Q4 2015
Q4 2015
Q4 2015
Q1 2016
Q2 2016
Q2 2016
Q2 2016
Q3 2016
Q3 2016
Q3 2016
Q3 2016
Q3 2016
Q4 2016
Q4 2016
Q4 2016
Q1 2017
Q1 2017
Q1 2017
Q2 2017
Q2 2017
Q2 2017
Q3 2017
Q3 2017
Q3 2017
Q1 2018
Q1 2018
Q1 2018
Q1 2018
Q1 2018
Q1 2018
Q3 2018
Q3 2018
Q3 2018
Q3 2018
Q3 2018
Q3 2018
Q3 2018
Q4 2018
Q4 2018
Q4 2018
Q4 2018
There are two rather obvious fail points. The first is Daedalus 9 which will have issues with the initial launch and be aborted (thus the N/A for -B and -C since the mission will scrub shortly after liftoff). The second is the 2nd launch for Daedalus 11 will be a total failure with destruction on the launch pad (thus the reason for the Daedalus 11-C abort as we won't be going to the moon with only half the equipment).
Roughly speaking its obviously a 2% chance for total failure and a 5% chance for emergency abort (counting Partial and Total Failure) and 10% chance for a mission scrub. From a safety standpoint I'm treating all Partial Successes as endangering the mission enough to require an abbreviated mission. I figure these are rather conservative numbers but much of that is from the speed into space and thus I'm treating the current launch system as needing a major shakeout.
The next major MSA programs will be:
Icarus (using the Ares VI system to go to the next closest planet)
Theseus (using the Jupiter/Delta IV to begin long term space habitation)
The Theseus program will have a much higher success rate indicating the maturation of the Jupiter and Delta IV systems. I will be switching to a =RANDBETWEEN(1,1000) with the rates set as TF 1-5, PF 6-10, PS 11-50, S 51-600, TS 601-1000. That would give me a 1% failure/emergency abort rate and a 4% mission abort rate. The Icarus program will have roughly the same sucess rates as above (the TF and PF are gonna drop a bit but PS will still be up to 15%) HOWEVER its going to get a lot more rolls (1 for each launch, 1 for initial burn, 1 for mid-course correction, 1 for orbital entry, 1 for going to the surface, 1 for coming up, 1 for TEI burn and 1 for mid-course correction). This means a typical mission without landings has 7 rolls and a lander mission 9.
Given that we are already in 2017 I'm going to indicate that Daedalus 6 did NOT land on the moon and the Daedalus 7 mission will be the landing. I'm assuming we switched to the 1 week= 1 month speed which would mean that Daedalus 7 will launch sometime between now and the end of the month, probably around next weekend if I remember otherwise the weekend after that.
Right now I'm trying for interesting dates and next weekend would give me roughly the 1st-8th of February and the weekend after that the same period in March so I may have to do it on the 1st or 2nd of next month in order to land on the Ides of March 2017.
*Edit* Had the old datestamps before the MSA pushed up the first few launches in Daedalus, datestamps are now current.
*Edit#2* I suddenly realized that if I was launching the Eagle as well on 13 and 14 that I should include 1 more roll for those missions so I added Daedalus 13-D and 14-D and re-rolled the missions (I upped the TF/PF but kept PS capped at 15).