 |
The airplane volume (3,4m У 3,2m У 14.1 Л), as well as the payload of experimental equipment, allocated in the laboratory compartment, advantageously single out our airplane from the similar ones in the world. The results of tests and experiments are registered by the standard on-board aircraft systems and additional test- and measuring equipment of the customer. The video- and photo-shooting are also available on board, as well as the subsequent processing of all the taken video- and photo- materials (if deemed necessary).
 |
Technical Data:
| Length of the airplane | 46.59 Л | |
| Height | 14.76 Л | |
| Wingspan | 50.50 Л |
Laboratory Compartment:
| Length of a floor | 24.18 m | |
| Width | 3.45 m | |
| Height | 3.40 m | |
| Overall payload dimensions | ||
| Length | 14.00 m | |
| Width | 3.30 m | |
| Height | 3.20 m | |
| Maximal payload | 10.00 tons | |
| Loading-and Unloading Equipment | 4 crabs with 2.5 tons capacity each | |
| Amount of participants | up to 20 persons | |
| Amount of parabolas in a single flight | up to 15 parabolas | |
| Duration of a parabola | about 28 seconds | |
| Residual G-load along longitudinal and vertical axes accordingly | X axis - 1У10-2 Y axis - 4У10-2 | |
| Flight duration | 1.5 - 2.0 hours | |
Power Supply:
| 3-phase current | 208/115 V, 400 Hz, 20 KW | |
| 3-phase current | 36 V, 400 Hz, 2 KW | |
| AC | 220 V, 50 Hz, 3 KW | |
| DC | 27 +/- 10%, 24 KW |
Lighting:
| 20 "SVET-1000" directional and scattered light lamps for laboratory compartment ( if color and white-&-black photo (video) is required ). | ||
| Number of lamps | 20 | |
| Axial light intensity of one lamp | not less than 15 000 lights | |
| Lamps operating mode | - continuously - preset time of operation | |
Auxiliary Radio Communication Equipment:
| Airplane's intercom system enables to maintain a telephone communication via two loops between the members of a safety team in the laboratory compartment (12 users at a time). |
Space Suit Pressurization and Ventilation Systemz:
|
Space suit pressurization and ventilation system provides for: - Simultaneous continuous ventilation and pressurization of four space suits aloft from the canisters, as well as continuous run the airplane's air conditioning system; - Air supply of each of 4 space suits (not less than 250 + /- 20 nl/min). |
Oxygen Supply System:
| This system provides additional emergency oxygen supply of free-floating crew members, test-engineers and investigators. 11 re-locatable oxygen sets are available on board. |
