Voici le cahier des charges pour le PPTS. Mais c'est une traduction automatique...en anglais!
Edit: voir plus loin dans le fil la traduction en français que j'ai faite 
Promis je ferai un résumé demain en français (là il est un peu tard).
Pour ceux que cela intéresse:
3.4.
The performance of requirements to designly-technical characteristics PPTS.3.4.1.
PPTS must cut in the flown ship of novel generation and developed to gv it base of modification.The base modification of flown ship is appointed for delivery 6 able-bodied man /person of crew and payload not less 500 kg gv orbital flown stations (OPS) and the recoveries of crew and payload not less 500 kg to earth.
The modifications of flown ship are appointed :
* For the delivery of crew by the crew size 4 able-bodied man /person and payload not less 100 kg gv circumlunar orbit, circumlunar orbital station and the recoveries of them to earth ;
* For experimentation and experimentation in autonomous manned mission by crew size till 4 able-bodied man /person (is fixed by terminal missions) by duration not less of 30 twenty four hours and it recovery ;
* For the transport-maintenance of низкоорбитальных automatic space crafts (KA), of platforms and autonomous moduluses, as well as in ensuring of convening of operations to removal from orbit faulted automatic KA and the major fragments of cosmic waste ,
* For rendering of commercial service in the context of cosmic tourism, for the delivery of stores not less 2000 kg gv OPS and the recoveries of stores not less 500 kg to earth in pilotless грузовозвращающей modification.
3.4.2.
The elements of orbit of the flight of the ship of base modification :
* The inclination of the orbital plane of flight _ 51.6 hail in flight to MICROSECONDS and 51.8 hail. In flight to OPS ;
* In delivery and the recovery of the crews of orbital stations _ 200 _ 500 km ;
* To study the fire hazard of the flight of the base modification of ship for the performance of terminal missions gv orbit with inclination planes - 73.2 hail.
3.4.3.
The ship onboard system must implement of all fly operations by common cosmonaut with the workspace. In ship should be of two равнозначных workspace contributing operation ship.
3.4.4.
Flight conditions for the crew of flown ship and it modifications must correspond requirements STATE STANDARD Live environment of cosmonaut in flown space craft. General medico-performance specification. Maneuvers, in operation gv crew, should be to about quatity :
* At stage of breeding to about conventional program _ not above 4.0 ед ;
* On-site conventional reentry in atmosphere _ not above 3.0 ед ;
* In reentry with peak cross range _ not above 5.0 ед ;
* In the mechanization of off-nominal situations _ not above 7.0 ед. (In breakaway from auxiliary RN in work SAS) and 12.0 ед. (Gv the weather effect part of reentry since last overhaul the completion of emergency rescue system).
3.4.5.
The fire hazard of making of safe landing in emergency reentry and the incidents of on-site breeding of the returned interphone control box (VA) at any time of year gv the not prepared site of land and gv distilled water.3.4.6.
The duration of autonomous flight :
* The base modification of flown ship and pilotless грузовозвращающей modification in servicing circumtellurian OPS _ not less of 5 twenty four hours ;
* Flown ships in servicing of automatic space crafts and platforms, in check-off to about breakaway from the orbit of faulted space crafts and the fragments of cosmic waste, the performance of terminal missions to about experimentation of and experimentation with спецаппаратурой, to developing of the technologies of strategic cosmic monitoring and cautions about large-scale emergency power situations of native and техногенного character, the decisions of missions double-track and militari-applied purpose not less of 30 twenty four hours ;
* In the utilization of the modification of flown ship for lunar operation with exit gv circumlunar orbit _ not less of 14 twenty four hours.
3.4.7.
The hold-up time of ships PPTS in the composition of flown stations :* In composition circumtellurian OPS _ not less of 1 year ;
* In composition circumlunar OPS _ not less of 200 twenty four hours.
3.4.8.
The stockage of the characteristic velocity of ships in check-off transport-maintenance must implement of dynamic operations, marriage, перестыковку and standby marriage with OPS, низкоорбитальными by automatic space crafts, platforms and autonomous moduluses, the performance of dynamic operations to reentry and ingress VA in the target area of surface of the earth.
3.4.9.
Test flight OPS serviced KA, of orbital platforms and moduluses, equipped by corresponding technical devices, and marriage with selected control port must be contributed in the automatic and manual engine power /thrust/ set of operation.3.4.10.
The precision of the ingress of returned interphone control box in conventional regime _ not worse 10 km for ensuring of ingress gv the area of Russia. Should be considered the various controls versions of ensuring of the given accuracy of ingress.
3.4.11. The flown ships of all modifications must contribute the rescue of crew gv all part of breeding, in water landing, the survival of crew till the arrival of the meanses researchly of-спасательного complex.
3.4.12. The level of dynamic loads in convening of dockings should not exceed strength properties and carrying capacity OPS, automatic KA, of orbital moduluses and the elements of their structures.
3.4.13. In the propulsion systems of man-manageable system, usable gv the weather effect part of flight, must be applied ecologically non-hazardous propellant components.
3.4.14. The ship original mass must let it breeding gv low datum orbit with inclination 51.8 hail. By rocket the-launcher of the middle class of higher lifting capacity (lifting capacity not less 20 т gv Nkr=200 km.).
3.4.15. The duration of the operation OF VA in case it manifold use _ not less 15 years old, the magnification degree /ratio of application _ till 10 flights.3.4.16.
The duration of the cycle of the preparation of ships PPTS to launching from the moment of delivery gv cosmodrome _ not above 30 twenty four hours.3.4.17.
Reliability and safety :
* The reliability of the program execution of the flight of ship in earth orbital flight or servicing of circumtellurian orbital station must compose not less 0.99 ;
* The mid-air collision poten of the safety of crew in earth orbital flight or servicing of circumtellurian orbital station must compose not less 0.995 ;
* In the process the operation of elements PPTS must be contributed the safety of ground personnel and cosmic infrastructure ;
* Resonant members, devices of and the onboard system of elements PPTS should be designed with allowance for stability requirement to two failures :
- In common failure flight programs is implement ;
- In two failures the crew rescue is contributed.
[Forum de NK]
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Sujet: PPTS: développement confié à Energia 
Ven 6 Mar 2009 - 22:18
