Report on Progress M-28M
To avoid anything written here causes the butterfly effect that jinxes the 60th Progress flight to the ISS, I'm not going to say anything except for the table below this time.
:rofl:
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+3)/
|
Universal / UTC
|
Washington / EDT (UTC-4)
Launch time (Primary):
|
14:55:50
|
10:55:50
|
07:55:50
|
04:55:50
|
00:55:50
on:
|
Jul. 3, 2015
|
Jul. 3, 2015
|
Jul. 3, 2015
|
Jul. 3, 2015
|
Jul. 3, 2015
Launch time (Backup):
|
14:07:35
|
10:07:35
|
07:07:35
|
04:07:35
|
00:07:35
on:
|
Jul. 5, 2015
|
Jul. 5, 2015
|
Jul. 5, 2015
|
Jul. 5, 2015
|
Jul. 5, 2015
{colsp=6}
[highlight][eventTimer]2015-07-03 04:55:50?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Progress M-28M Launch[/highlight]
{colsp=5}Docking times
Time Zone
|
Australia - Sydney/AEST (UTC+10)
|
Moscow / MSKS (UTC+3)/
|
Universal / UTC
|
Washington / EDT (UTC-4)
Docking time (Primary):
|
17:13:02 ±3 min
|
10:13:02 ±3 min
|
07:13:02 ±3 min
|
04:13:02 ±3 min
on:
|
Jul. 5, 2015
|
Jul. 5, 2015
|
Jul. 5, 2015
|
Jul. 5, 2015
Docking time (Backup):
|
15:28 ±3 min
|
08:28 ±3 min
|
05:28 ±3 min
|
01:28 ±3 min
on:
|
Jul. 7, 2015
|
Jul. 7, 2015
|
Jul. 7, 2015
|
Jul. 7, 2015
{colsp=5}
[highlight][eventTimer]2015-07-05 10:13:02?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Progress M-28M docking to ISS[/highlight]
Live Coverage Of The Launch:
Progress M-28M (industry id 11F615A60 #428, NASA id Progress 60P) cargo spaceship
Cargo Manifest
Code:
Total mass of spacecraft at launch 7282 kg
Propellants for the propulsion system (KDU) 880 kg
Propellants in the refueling system 520 kg
Air 22 kg
Oxygen 26 kg
Water in Rodnik ("Creek") system tanks 420 kg
Pressured section cargo (total mass 1393 kg)
Equpiment for systems:
* SOGS atmosphere composition control 12 kg
* SVO water supply control 38 kg
* SOTR heat exchange control 10 kg
* STOR maintenance and repair 30 kg
* SUBA control system accessories 6 kg
* SEP power control 105 kg
* KSPE crew support equipment 44 kg
* BITS2 on-board information and telemetry system 1 kg
* MBRL antenna connectors 3 kg
*SGO Hygiene and sanitation items 273 kg
*Food rations, fresh products 430 kg
*Medical equipment, underwear,
personal hygiene and care, station
air purity checking and cleaning 137 kg
*Crew support equipment 44 kg
*Science experiments and apparatus
equipment 21 kg
*Maintenance equipment 3 kg
*FGB Zarya equipment 39 kg
*US Segment equipment 55 kg
*US goods for Russian crew 186 kg
Total cargo mass 2381 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: 08:04:39.18
2. Orbital Parameters of Progress M-28M and the ISS
Parameter|Designation|Prorgess-M-28M on 7/3|ISS on 7/5
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
338.8 degrees
Projected life time 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
03.07.15|11:36:07|3|15.63|40.0|89.11|51.65|216.9|258.1
03.07.15|11:59:35|3|22.94|57.7|89.91|51.65|256.4|304.5
* 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
04.07.15|09:40:11|18|2.00|29.3|89.96|51.64|261.3|303.5
Autonomous approach program is initiated at 07:51:02.
4. Approach at the Close range
Fly-around, station keeping and docking procedures will be used on July 5, 2015 from 09:51:20 ±3 min to docking contact
5. Docking
Contact and capture will be performed on July 5, 2015 at 10:13:02 ±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/log2015.html#rate:
Code:
================================================================
Vehicle Successes/Tries Realzd Pred Consc. Last Dates
Rate Rate* Succes Fail
================================================================
Soyuz-U 751 771x .97 .97 14 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 July 3, 2015 (11 a.m.)
Plentiful sunshine. High near 35C. Winds NW at 15 to 30 km/h.
Time|Temps|Dew Point|Relative Humidity|Precip|Snow|Cloud cover|Pressure|Wind|Weather
11 AM|32°C|10°C|25%|0%|0%|0%|1010 hPa|19 km/h NW|
Clear
