Progress M-19M mission report
Note that Progress M-19M was switched from the 6 hour launch-to-docking profile back to the standard 2 day flight to the ISS, because the launch team at Baikonur cannot support the 6 hour launch-to-docking profile launch window (which came on April 22) after supporting the Bion-M launch last week.
Launch location:
Baikonur Launch pad no. 1/5 45°55'12.85"N, 63°20'32.27"E
Launch dates and times:
{colsp=6}Launch times
Time Zone
|
Australia - Sydney/AEDT (UTC+12)
|
Baikonur / UTC+6
|
Moscow / MSKS (UTC+4)/
|
Universal / UTC
|
Washington / EDT (UTC-4)
Launch time (Primary):
|
22:12:16
|
16:12:16
|
14:12:16
|
10:12:16
|
06:12:16
on:
|
Apr. 24, 2013
|
Apr. 24, 2013
|
Apr. 24, 2013
|
Apr. 24, 2013
|
Apr. 24, 2013
Launch time (Backup):
|
21:49:43
|
15:49:43
|
13:49:43
|
09:49:43
|
05:49:43
on:
|
Apr. 25, 2013
|
Apr. 25, 2013
|
Apr. 25, 2013
|
Apr. 25, 2013
|
Apr. 25, 2013
{colsp=6}
[highlight][eventTimer]2013-04-24 10:12:16?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Progress M-19M Launch[/highlight]
{colsp=6}Docking times
Time Zone
|
Australia - Sydney/AEDT (UTC+12)
|
Moscow / MSKS (UTC+4)/
|
Universal / UTC
|
Washington / EDT (UTC-4)
Docking time (Primary):
|
00:26:18 ±3 min
|
16:26:18 ±3 min
|
12:26:18 ±3 min
|
08:26:18 ±3 min
on:
|
Apr. 27, 2013
|
Apr. 26, 2013
|
Apr. 26, 2013
|
Apr. 26, 2013
Docking time (Backup):
|
23:38 ±3 min
|
15:38 ±3 min
|
11:38 ±3 min
|
07:38 ±3 min
on:
|
Apr. 27, 2013
|
Apr. 27, 2013
|
Apr. 27, 2013
|
Apr. 27, 2013
{colsp=6}
[highlight][eventTimer]2013-04-26 12:26:18?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Progress M-19M docking to ISS[/highlight]
Live Coverage Of The Launch:
Progress M-19M (industry id 11F615A60 #419, NASA id Progress 51P) cargo spaceship
Cargo Manifest
Code:
Propellants in the refueling system 365 kg
* Oxygen 26 kg
* Air 22 kg
Water in Rodnik ("Creek") system tanks 410 kg
Pressured section cargo (total mass 1543 kg)
Equpiment for systems:
* SOGS atmosphere composition control 83 kg
* SVO water supply control 120 kg
* SOTR heat exchange control 8 kg
* SKASh acoustic noise control system 1 kg
* STOR maintenance and repair 6 kg
* KS TOR maintenance and repair kit 27 kg
SPPZ fire protection system items 6 kg
SGO Hygiene and sanitation items 118 kg
Food rations, fresh products 198 kg
Medical equipment, underwear,
personal hygiene and care, station
air purity checking and cleaning 695 kg
FGB Zarya equipment 62 kg
MRM-1 Rassvet equipment 10 kg
MRM-2 Poisk equipment 19 kg
DC-1 Pirs equipment 18 kg
Scientific equipment for experiments 21 kg
Technological support equipment 16 kg
Personal delivery for Russian
crew members 103 kg
Photography equipment for crew members 33 kg
American food rations delivery 15 kg
Total cargo mass 2366 kg
Mission Profile
Ascent Chart:
1. Approach and Docking Chart:
The times below are in Moscow Standard Time (UTC+4):
The expected payload separation time: 14:21:06.18
2. Orbital Parameters of Progress M-19M and the ISS
Parameter|Designation|Prorgess-M-19M on 04/24|ISS on 04/26
Orbital Period|T, min|88.59 ±0.37|92.69
Inclination|i, degrees|51.66 ±0.06|51.66
Min altitude|h, km|193 +7 -15|402.85
Max altitude|H, km|245 ±42|426.87
Phase angle between the space ship and the ISS is about
231 degrees
Projected duration of the space ship at the nominal orbit is no less than 20 orbits (~30 hrs)
3. Transfer manoeuvres
(two days long approach scheme applied)
* Nominal two-burn manoeuvre forming a phasing orbit
Date|Burn at|Orbit #|Delta V, m/s|Burn duration, s|post-burn T,min|post-burn i,deg|post-burn h,km|post-burn H,km
24.04.13|17:53:36|3|41.45|97.00|90.00|51.64|230.11|334.30
24.04.13|18:45:32|4|26.57|61.9|90.94|51.63|291.29|362.49
* The 2nd day's one-burn correction
Date|Burn at|Orbit #|Delta V, m/s|Burn duration, s|post-burn T,min|post-burn i,deg|post-burn h,km|post-burn H,km
25.04.13|15:36:06|17|2.00|29.0|91.00|51.66|297.98|361.77
Autonomous approach program is initiated at 14:03:15.
4. Approach at the Close range
Fly-around, station keeping and docking procedures will be used on April 26, 2013 from 16:02:52 ±3 min to docking contact
5. Docking
Contact and capture will be performed on April 26, 2013 at 16:26:18 ±3 min
Docking is to SM Zvezda +X docking port
Launch Vehicle:
{colsp=2}Characteristics
|
{colsp=2}
Soyuz-U
Prime contractor:
|
- Samara Space Sentre (Energia Holding enterprise)
GRAU Index:
|
Height:
| 51.1 m
Diameter:
| max 10.3 m
Liftoff mass:
| 313 metric tonnes
Payload mass:
| 6.95 tonnes at ISS orbit from Baikonur
1st stage (boosters B, V, G, D):
|
- 4 X RD-117 engines
- Propellants (T-1 Kerosene and LOX)
- Thrust/ISP in vacuum - / 316 s
- Thrust/ISP at sea level 79.4 tonnes / 253 s
- Total 1st stage's thrust at sea level: 411.1 tonnes
2nd stage (core A):
|
- 1 X RD-118 engine
- Propellants (T-1 Kerosene and LOX)
- Thrust/ISP in vacuum 102 tonnes / 314 s
- Thrust/ISP at sea level 83.5 tonnes / 257 s
3rd stage (block I):
|
- 1 X RD-0110 engine
- Propellants (T-1 Kerosene and LOX)
- Thrust/ISP in vacuum 30.38 tonnes / 359 s
The vehicle's
reliability statistics according to
http://www.spacelaunchreport.com/log2013.html#rate:
Code:
================================================================
Vehicle Successes/Tries Realzd Pred Consc. Last Dates
Rate Rate* Succes Fail
================================================================
Soyuz-U 743 763x .97 .97 6 8/24/11 1973-
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.