Report on Progress M-23M
"Hello? Yes this is ISS FE7 calling Houston.....yeah you know we need a part to repair the oxygen recycling rack......it's on CRS-3? Ah OK it should be shipped by mid-Mar......what? Grounded? There's contamination on the trunk? Ah OK it has been cleared.....now what? Another delay? A radar caught fire at the Cape? Oh @#*$......."
:facepalm: :rofl:
Well of course this isn't happening in real life, but the logistics to and from the ISS has always been in a state of flux since its very beginning, subjected to a huge number of constraints that affects the launch and landing schedules of visiting vehicles and requires constant attention for those working on ISS work plan scheduling (e.g. at MCC-H and MCC-M). (see Dragon CRS-3 and Cygnus CRS-2 for recent examples -
the later of which may be grounded till mid-June due to delays with the former)
However there's one vehicle that seems to (at least in most cases) defy this law and seems to be working reliably and almost always on schedule for orbital delivery - the Progress. And while we are still waiting for the next Dragon to finally depart, another Progress is already now waiting to fly to the ISS! Progress M-23M is the 145th Progress to fly since 1978, and as with most of the others will carry more than 2.3 tonnes of cargo to the station - interestingly about the mass of the cargo lifted by the last Dragon and Cygnus combined.
So here are the details: :tiphat:
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/AEST (UTC+10)
|
Baikonur / UTC+6
|
Moscow / MSKS (UTC+4)/
|
Universal / UTC
|
Washington / EDT (UTC-4)
Launch time (Primary):
|
01:26:25
|
21:26:25
|
19:26:25
|
15:26:25
|
11:26:25
on:
|
Apr. 10, 2014
|
Apr. 9, 2014
|
Apr. 9, 2014
|
Apr. 9, 2014
|
Apr. 9, 2014
Launch time (Backup):
|
00:41:18
|
20:41:18
|
18:41:18
|
14:41:18
|
10:41:18
on:
|
Apr. 12, 2014
|
Apr. 11, 2014
|
Apr. 11, 2014
|
Apr. 11, 2014
|
Apr. 11, 2014
{colsp=6}
[highlight][eventTimer]2014-04-09 15:26:25?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Progress M-23M Launch[/highlight]
{colsp=6}Docking times
Time Zone
|
Australia - Sydney/AEST (UTC+10)
|
Moscow / MSKS (UTC+4)/
|
Universal / UTC
|
Washington / EDT (UTC-4)
Docking time (Primary):
|
07:20:13 ±3 min
|
01:20:13 ±3 min
|
21:20:13 ±3 min
|
17:20:13 ±3 min
on:
|
Apr. 10, 2014
|
Apr. 10, 2014
|
Apr. 9, 2014
|
Apr. 9, 2014
Docking time (Backup):
|
03:03 ±3 min
|
21:03 ±3 min
|
17:03 ±3 min
|
13:03 ±3 min
on:
|
Apr. 14, 2014
|
Apr. 13, 2014
|
Apr. 13, 2014
|
Apr. 13, 2014
{colsp=6}
[highlight][eventTimer]2014-04-09 21:20:13?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Progress M-23M docking to ISS[/highlight]
Live Coverage Of The Launch:
Progress M-23M (industry id 11F615A60 #427, NASA id Progress 55P) cargo spaceship
Cargo Manifest
Code:
Total mass of spacecraft at launch 7280 kg
Propellants for the propulsion system (KDU) 880 kg
Propellants in the refueling system 700 kg
Oxygen 22 kg
Air 26 kg
Water in Rodnik ("Creek") system tanks 420 kg
Pressured section cargo (total mass 1215 kg)
Equpiment for systems:
* SOGS atmosphere composition control 9 kg
* SVO water supply control 90 kg
* SOTR heat exchange control 23 kg
* STOR maintenance and repair 4 kg
* SUDN spacecraft navigation and rendezvous control system 14 kg
* MBRL communication antenna 4 kg
* EKTS power cables 53 kg
* KS TOR maintenance equipment 1 kg
*SGO Hygiene and sanitation items 361 kg
*Food rations, fresh products 367 kg
*Medical equipment, underwear,
personal hygiene and care, station
air purity checking and cleaning 81 kg
*Personal protection equipment 20 kg
*Photography and video equipment 16 kg
*Science experiments and apparatus
equipment 27 kg
*FGB Zarya equipment 4 kg
*MRM-2 Poisk equipment 9 kg
*Personal delivery for Russian
crew members 132 kg
Total cargo mass 2383 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: 19:35:16.18
2. Orbital Parameters of Progress M-23M and the ISS
Parameter|Designation|Prorgess-M-23M on 4/9|ISS on 4/10
Orbital Period|T, min|88.59 ±0.37|92.78
Inclination|i, degrees|51.66 ±0.06|51.66
Min altitude|h, km|193 +7 -15|411.21
Max altitude|H, km|245 ±42|432.19
Phase angle between the space ship and the ISS is about
25.4 degrees
Projected duration of the space ship at the nominal orbit is no less than 20 orbits (~30 hrs)
3. Transfer manoeuvres
(six hours 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
09.04.14|20:12:16|1|35.49|88.8|89.81|51.63|233.4|313.9
09.04.14|20:55:05|2|30.50|75.6|90.88|51.64|312.4|346.6
09.04.14|21:30:15|2|7.00|18.3|91.13|51.67|324.9|357.9
09.04.14|22:00:40|2|7.00|18.3|91.37|51.64|345.1|359.5
Autonomous approach program is initiated at 23:12:45.
4. Approach at the Close range
Fly-around, station keeping and docking procedures will be used on April 10, 2014 from 00:57:30 ±3 min to docking contact
5. Docking
Contact and capture will be performed on April 10, 2014, 2014 at 01:20:13 ±3 min
Docking is to DC-1 Pirs -Y 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/log2014.html#rate:
Code:
================================================================
Vehicle Successes/Tries Realzd Pred Consc. Last Dates
Rate Rate* Succes Fail
================================================================
Soyuz-U 747 767x .97 .97 10 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.
Weather forecast for Baikonur, Kazakhstan on April 9, 2014 (9 p.m.)
Showers this evening, becoming a steady rain overnight. Low 8C. Winds W at 10 to 15 km/h. Chance of rain 60%.
Time|Temps|Dew Point|Relative Humidity|Precip|Snow|Cloud cover|Pressure|Wind|Weather
9 PM|14°C|9°C|75%|50%|0%|97%|1004 hPa|6 km/h SW|
Chance of rain