Project Updated Phobos-Grunt

[ron-111]

This is my first addon

Meshes are ready for 65%


*UPDATE*
with mdu, adapter and YH-1


*UPDATE*
texturing


*UPDATE*
arriving to Mars


*UPDATE*
thx to SiberianTiger for help:thumbup:

in Mars initial orbit


P.S. after orbit insertion we have only 64 kg of fuel left in MDU:lol:


Release is coming!!!

P.S. sorry for bad english

 

[dgatsoulis]

Have a look at SiberianTiger's post here.

 

[ron-111]

Have a look at SiberianTiger's post here.

Cruise Stage mass = 550 + 180 = 730? or dry mass of propulsion system already included in Cruise Stage mass(550)?

 

[dgatsoulis]

I think that it's the first one (550+180), but I can't find another source to confirm it.

 

[SiberianTiger]

The masses breakdown of Phobos-Grunt spacecraft according to the table given in Novosti-Kosmonavtiki magazine (1/2012):

Part|Mass, kg
Descent Module|7
Return Vehicle, including:|287
- propellants|139
- dry mass|148
Cruise Stage Avionics Module|550
Cruise Stage Propulsive Module, including:|1270
- propellants|1058
- dry mass|212
Interstage Truss with Separation Devices|150
Chinese Subsatellite|115
Propulsive Stage without Auxiliary Tanks, including:|7750
- propellants|7015
- dry mass|735
Auxiliary Tanks, including:|3376
- propellants|3001
- dry mass|375
TOTAL|13505

 

[ron-111]

on mars arriving in MDU is 500 kilograms of propellant only
and we can not make a orbit insert

 

[SiberianTiger]

on mars arriving in MDU is 500 kilograms of propellant only
and we can not make a orbit insert

Potentially, with a perfect picking of approach trajectory, you can make an orbit insert even without spending any propellants at all (the planet will "capture" you from a fly-by trajectory). If you need specific details of PhG's flight plan you can't find on the Internet, let me know.

 

[ron-111]

If you need specific details of PhG's flight plan

yes please

 

[SiberianTiger]

Okay, so this is what was there in Phobos-Grunt's happy afterlife...

When|Burn delta-V|Burn Time|Orbit achieved|Comments
{colsp=5}

Earth departure, Trans-Mars Injection​

2011-09-08 23:27|-|-|207.0 x 347.0 X 51.48° Earth|Parking orbit
2011-09-09 01:57|830 m/s|505.3 s|244.4±6 x 4162.0±14 x 51.44°±7.5' T=131.7m Earth|Intermediate orbit, aux tank jettison
2011-09-09 04:04|2900 m/s|976.1 s|Escape e=1.153251, h=423.6±10, i=51.43°±0.33°, asymptote velocity ≤ 3.1 km/s, equ apex declination ≤ 40°|TMI
{colsp=5}

Mars Transfer​

5-10 days after dep|≤ 85 m/s|?|Transfer|Correction 1
65 days after dep|≤ 10 m/s|?|Transfer|Correction 2
4-2 weeks before arr|≤ 35 m/s|?|Transfer|Correction 3
{colsp=5}

Mars Orbit Insertion, asym. vel of arrival ≤ 2.8 km/s, equ apex declination ≤ 30°​

2012-08-25 - 2012-09-26|945 m/s|2.2 m|800±400 x 79000 Mars|Initial orbit in the plane of arrival, jettison of MDU, Yinho, Truss
10-15 days after|220 m/s|4.8 m|9910 x 79000 in plane of Phobos, Mars|Apogee burn, also plane alignment with Phobos
When in periapsis|705 m/s|12.3 m|9910 x 9910 in plane of Phobos, T=8.3 hrs, Mars|Observation orbit, few corrections here
Some time after|45 m/s + 20 m/s|?|50 x 130 Quasi-Sync orbit ot Phobos|Approach Orbit
{colsp=5}

Phobos landing​

5 days after|100 m/s|spread over 2 hrs|Landed either at 5°S 235°W or 5°N 230°W|Landing speed 1.0-2.5 m/s vertical, 1.0 m/s lateral
{colsp=5}

Phobos Departure​

Year 2013|1 m/s|0|up vertical from Phobos|Spring action
50-60 s later|10 m/s|16 s|up vertical from Phobos|Clearing burn
1000 s later|20 m/s|32 s|towards the Sun, Mars-centric orbit achieved|Automatic takeoff orbit
3 days after|20 m/s|?|Mars-centric 300-350 km lower than Phobos', T=7.23 hours|Staging orbit for launch window awaiting
{colsp=5}

Trans-Earth Injection​

3-23 September, 2013|740 m/s|?|Elliptic 3 days T Mars|Raising apoapsis
When in apoapsis|125 m/s|?|Periapsis lowered by 500-1000 km, inclination changed|Targeting orbit
When in periapsis|790 m/s|?|Escape, asymptote velocity ≤ 2.5 km/s, equ apex declination -3° ... -6°|TEI
{colsp=5}

Earth Transfer, allows for 5 corrections, totaling ≤ 140 m/s​

{colsp=5}

Earth Landing, at 46°01'N, 72°10'E, entry angle 33...45° at 120 km.​

 

[ron-111]

:blink: WTF in orbiter Phobos has Pe=5853km and Ap=6161km BUT here http://en.wikipedia.org/wiki/Phobos_(moon) is write that Ap=9518km and Pe=9235km ?????? WTF
:facepalm:

 

[asbjos]

:blink: WTF in orbiter Phobos has Pe=5853km and Ap=6161km BUT here http://en.wikipedia.org/wiki/Phobos_(moon) is write that Ap=9518km and Pe=9235km ?????? WTF
:facepalm:

Possibly because that the apoapsis and periapsis in Wikipedia is mesaured from the center of Mars. Just take 9235 (Perigee mesaured from center) - 3396 (planet radi) = 5839, very close to your PeA

 

[ron-111]

UP!

I came back and continued to work on addon :thumbup:
I am pleased to announce that BETA2 released
[ame="http://www.orbithangar.com/searchid.php?ID=5748"]Updated Phobos-Grunt(BETA 2)[/ame]

 

[Thorton]

Please remove from your addon Fregat mesh, which you take from my Soyuz FG addon. I didnt give you permission to use it.

 

[ron-111]

Please remove from your addon Fregat mesh, which you take from my Soyuz FG addon. I didnt give you permission to use it.

ok

[ame="http://www.orbithangar.com/searchid.php?ID=5748"]Updated Phobos-Grunt(BETA 3)[/ame]