Author Topic: A Different Take On Reliability  (Read 36425 times)

Offline edkyle99

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Re: A Different Take On Reliability
« Reply #60 on: 04/25/2022 01:30 pm »

================================================================
                   
        ACTIVE LAUNCH VEHICLE RELIABILITY STATISTICS
================================================================
           by Ed Kyle      as of April 21, 2022     
================================================================
Top active space launch vehicles ranked by Lewis point estimate
of their orbital success rate*.  Failures include incorrect
orbits.
================================================================
                           Lewis
                Successes  Point AdjWald   Consc. Last    Dates
Vehicle         /Attempts  Est*  95%CI*    Succes Fail   
================================================================
Falcon 9 v1.2    128/128(D)0.99  0.96-1.00 128   None     2015-
Atlas 5           91/92    0.98  0.94-1.00  82   06/15/07 2002-
CZ-2D             57/58    0.97  0.90-1.00  26   12/28/16 1992-
Ariane 5-ECA(+)   77/79    0.96  0.91-1.00  14   01/25/18 2002-
H-2A              44/45    0.96  0.87-1.00  39   11/29/03 2001-
CZ-4(A/B/C)       87/90    0.96  0.90-0.99  29   05/22/19 1988-
CZ-2(C)(/SD/SM/YZ)62/64    0.95  0.89-1.00  28   08/18/11 1974-
CZ-3B/3C          98/102   0.95  0.90-0.99  18   04/09/20 1996-
CZ-2F(T/Y/G)      16/16    0.94  0.77-1.00  16   None     1999-
Soyuz 2-1a        29/30#   0.94  0.82-1.00  23   04/28/15 2004-
Soyuz 2-1b/Fregat 57/60    0.94  0.86-0.99  30   11/28/17 2006-
Soyuz 2-1a/Fregat 28/29#   0.94  0.81-1.00  26   05/21/09 2006-
Soyuz 2-1b        13/13    0.93  0.73-1.00  13   None     2008-
Minotaur 1        12/12    0.93  0.72-1.00  12   None     2000-
CZ-11             12/12    0.93  0.72-1.00  12   None     2015-
PSLV              51/54    0.93  0.84-0.99  13   08/31/17 1993-
Antares 2xx       11/11    0.92  0.70-1.00  11   None     2016-
CZ-3/3A           37/40    0.90  0.79-0.98  27   08/18/96 1984-
CZ-6               8/8     0.90  0.63-1.00   8   None     2015-
Vega              17/19xx  0.89  0.67-0.98   3   11/17/20 2012-
Proton-M/Briz-M   90/100   0.89  0.82-0.94   0   12/13/21 2001-
Pegasus (H/XL)    40/45    0.89  0.76-0.96  31   11/04/96 1991-
Electron          22/25    0.88  0.69-0.97   5   05/15/21 2017-
Kuaizhou 1(A)     14/16    0.88  0.63-0.98   0   12/15/21 2013-
Minotaur 4/5       6/6++   0.88  0.56-1.00   6   None     2010-
Delta 4 Heavy     12/13    0.87  0.65-1.00  12   12/21/04 2004-
Epsilon            5/5     0.86  0.51-1.00   5   None     2013-
CZ-7               4/4     0.83  0.45-1.00   4   None     2016-
GSLV Mk3           3/3z    0.80  0.38-1.00   3   None     2017-
Falcon Heavy       3/3     0.80  0.38-1.00   3   None     2018-
Soyuz 2-1v/Volga   4/5     0.80  0.36-0.98   3   12/05/15 2013-
CZ-5               4/5     0.80  0.36-0.98   3   07/02/17 2016-
Shavit(-1,-2)      9/12    0.75  0.46-0.92   5   9/6/04   1988-
GSLV Mk2           6/8     0.75  0.40-0.94   0   08/12/21 2010-
Soyuz 2-1v         2/2     0.75  0.29-1.00   2   None     2018-
Angara A5/Briz-M   2/2     0.75  0.29-1.00   2   None     2014-
CZ-5B              2/2     0.75  0.29-1.00   2   None     2020-
Ceres-1            2/2     0.75  0.29-1.00   2   None     2020-
CZ-8               2/2     0.75  0.29-1.00   2   None     2020-
Qased              2/2     0.75  0.29-1.00   2   None     2020-
LauncherOne        3/4     0.75  0.29-0.97   3   05/25/20 2020-
Taurus (XL)        7/10    0.70  0.39-0.90   1   3/4/11   1994-
CZ-7A              2/3     0.67  0.20-0.94   2   03/16/20 2020-
CZ-6A              1/1     0.67  0.17-1.00   1   None     2022-
Proton M           1/1     0.67  0.17-1.00   1   07/21/21 2021-
Soyuz 2-1a/Volga   1/1     0.67  0.17-1.00   1   None     2016-
KT-2               1/1     0.67  0.17-1.00   1   None     2017-
Jielong-1          1/1     0.67  0.17-1.00   1   None     2019-
Proton-M/DM-03     3/5     0.60  0.23-0.88   3   07/02/13 2010-
Safir              5/9(C)  0.56  0.27-0.81   0   02/05/19 2008-
SS-520             1/2     0.50  0.09-0.91   1   01/14/17 2017-
Unha (TD-2)        2/5%    0.44  0.12-0.77   2   04/12/12 2006-
SQX-1              1/3     0.43  0.06-0.80   0   08/03/21 2019-
Astra Rocket 3     2/6     0.40  0.09-0.70   1   02/10/22 2020-
Angara A5/Persei   0/1     0.40  0.00-0.83   0   12/27/21 2021-
KSLV-2 (Nuri)      0/1     0.40  0.00-0.83   0   10/21/21 2021-
KZ-11              0/1     0.40  0.00-0.83   0   07/10/20 2020- 
ZQ-1               0/1     0.40  0.00-0.83   0   10/27/18 2018-
OS-M               0/1     0.40  0.00-0.83   0   03/27/19 2019-
Alpha              0/1     0.40  0.00-0.83   0   09/03/21 2021-
Simorgh            0/4(E)  0.28  0.00-0.62   0   12/31/21 2017-
================================================================
* Lewis Point Estimate Determined as Follows.
 
  Maximum Liklihood Estimate (MLE)= x/n
      where x=success, n=tries
  For MLE<=0.5, use Wilson Method = (x+2)/(n+4)
  For MLE Between 0.5 and 0.9, use MLE = x/n
  For MLE>=0.9, use Laplace Method = (x+1)/(n+2)
 
  Lewis, J. & Lauro, J., "Improving the Accuracy of Small-Sample
   Estimates of Completion Rates", Journal of Usability Studies,
   Issue 3, Vol. 1, May 2006, pp. 136-150.

* Adjusted-Wald 95% Confidence Interval Range Determined
     as Follows.

     Pw = (x+1.9208)/(n+3.8416)

     CI = Pw +/- 1.96*sqrt[(Pw*(1-Pw))/(n+3.8416)] 
          (maximum range 1.00)
   
# Does not include one successful suborbital Soyuz 2-1a test
   flight performed in 2004.

++Does not include two successful suborbital Minotaur 4 Lite
   flights in 2010-11.

x Does not include Soyuz-U/Soyuz T-10-1 pre-launch fire that
   resulted in escape tower firing saving crew, but destroying
   launch vehicle on 9-26-1983.  Note that 10 additional
   Soyuz-U launches with Ikar or Fregat upper stages (all
   successful) are cataloged separately.

xx Does not include successful 2-11-15 suborbital flight with
    IXV reentry demonstrator.

% Includes 2006 failure thought to be a two-stage suborbital
   test launch attempt.

z Does not include successful inaugural suborbital test flight
    on 12-18-14.

(C) Assumes that two unsuccessful, unreported Safir launch
     attempts occurred during 2012 and one during 2019.
     Does not count 2019 prelaunch propellant loading explosion.
 
(D) Does not include 09/01/16 explosion that destroyed F9-29
     and AMOS 6 payload during propellant loading for prelaunch
     hot fire test at CC 40 two days before planned launch.     
(D) Does not include successful 01/19/20 suborbital IFA Crew
     Dragon launch by F9-80. 

(E) Assumes 7/27/17 launch was a failed orbital attempt and
     that 4/19/16 launch was a suborbital test flight. 
       

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