- Joined
- Feb 13, 2008
- Messages
- 5,398
- Reaction score
- 8
- Points
- 0
- Location
- Khimki
- Website
- tigerofsiberia.livejournal.com
Mission: Supply run to the ISS replenishing onboard reserves of fuels, food, water and other consumables essential for continued manned flight of the complex
The launch site: Baikonur
The launch time is:
00:37:09 Baikonur 08.05.2009
22:37:09 MDT 07.05.2009
18:37:09 UTC May 7, 2009
2:37:09 p.m. EDT May 7, 2009
The expected docking time is:
23:22±3 min MDT 12.05.2009
19:22±3 min UTC May 12, 2009
3:22 p.m. ±3 min EDT May 12, 2009
Spacecraft: Progress M-02M (production #402)
The M-02M is the 2nd specimen of the new modification of Progress series spacecrafts with upgraded avionics. The spacecraft's mass is 7290.0 kg
Cargo manifest:
Code:
Refueling system propellants amount 870 kg
Oxygen 51 kg
Self fuel reserve available for the ISS 250 kg
Pressured section cargo (total mass 1339 kg)
Equpiment for systems:
SOGS gas mixture composition control 45 kg
SVO water supply control 53 kg
SOTR heat exchange conrtol 6 kg
SUBA equipment control 30 kg
SUDN flight and navigation control 48 kg
STOR maintenance and repair items 7 kg
Hygiene and sanitation items 104 kg
Food rations, fresh products 178 kg
Medical equipment, underwear,
personal hygiene and care 133 kg
SIZ personal protection, including
Orlan-MK space suit 195 kg
FGB [I]Zarya[/I] equipment 65 kg
SO1 [I]Pirs[/I] equipment 1 kg
Scientific equipment (for Tiplologia,
Pilot, Matryoshka-R experiments) 4 kg
Onboard documentation, crew parcel,
video and photo equipment 15 kg
American Sergent delivery, including
food rations, life support means,
medical, personal hygiene and care means,
zero 6 prophylaxis means 466 kg
All cargo total mass 2590 kg
Mission Profile:
1. Soyuz-U's ascent chart
2. Initial orbit's parameters
The expected payload separation time: 22h 45m 55.18s
Code:
Progress M-02M The ISS
Orbit Parameter Designation Nominal value and tolerance limits At the alignment orbit
Period T, min 88.59 ±0.37 91.50
Minimum altitude h, km 193.0 +7 -15 344.9
Maximum altitude H, km 245.01 ±42 368.9
Inclination i, degrees 51.66 ±0.06 51.66
Projected duration of the space ship at the nominal orbit is no less than 20 orbits (~30 hrs)
3. Transfer manoeuvres
(five days long approach scheme applied)
3.1. Orbit Phasing by the pre-calculated ballistic information
* 1st one-burn engine test manoeuvre
Code:
Expected orbit post burn
Date Burn at Orbit # Delta V, m/s Burn duration, s T,min h,km H,km i,deg
08.05.09 03.13.34 4 5.00 13.7 88.75 193.6 261.1 51.62
Code:
Expected orbit post burn
Date Burn at Orbit # Delta V, m/s Burn duration, s T,min h,km H,km i,deg
08.05.09 21.27.56 16 31.99 80.1 89.82 225.6 313.4 51.65
08.05.09 22.11.51 17 26.68 194.9 90.75 296.9 354.5 51.65
Code:
Expected orbit post burn
Date Burn at Orbit # Delta V, m/s Burn duration, s T,min h,km H,km i,deg
11.05.09 20.57.37 63 3.00 43.6 90.85 305.7 353.9 51.64
Code:
Expected orbit post burn
Date Burn at Orbit # Delta V, m/s Burn duration, s T,min h,km H,km i,deg
12.05.09 21.11.09 79 2.64 7.7 90.94 314.2 354.2 51.64
12.05.09 21.56.33 80 3.01 8.6 91.05 314.2 363.9 51.64
Launch preparation picture chronicles
06-04-2009 Preparatory works at Baikonur
16-04-2009 Zvezda Company's specialists test Orlan-MK space suit to be delievered
20-04-2009 Orlan-MK space suit is being prepared for delivery to the ISS
Last edited: