Решетневские чтения: Материалы xiii Международной...

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102

. 1.

. 2.

R. F. Aglyamov, E. S. Litvinov, O. V. Tselischev

Ufa State Aviation Technical University, Russia, Ufa

SOLID-PROPELLANT ROCKET The subject of research is a rocket engine with the deep control of thrust module and multirepeated starting

for the transporting space rocket systems. Using the method of the damping control the fuel burning surface with the liquid coolant will afford to operate the rocket engine more efficiently.

. ., . ., . ., 2009

669.713.7

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- - , - , - .

V. A. Vinogradov, V. I. Valov

Chemical plant branch of JSC Krasnoyarsk Machine-Building Plant, Russia, Podgorny

FEATURES OF PREPARATION AND CARRYING OUT FIRE AND COLD TESTS OF LIQUID ROCKET ENGINES ON THE CHEMICAL

PLANT BRANCH OF JSC KRASNOYARSK MACHINE-BUILDING PLANT The general testing stand organization is described, the problems connected with renovation of testing com-

plex facilities are considered, the requirements to testing personnel are specified.

. ., . ., 2009

104

523.9-1/-8

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. -

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105

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, - - - .

1. , . . / . . // . , 2004. 2 (18).

2. , . . , / . . // : XI . . . ; . . . -. -, 2007.

3. , . . / . . // . , 2007. 1 (29).

4. GreenWord [ ]. : http://greenword.ru. . .

5. , . . - / . . . . : , 1974.

N. V. Danilenko

Irkutsk Higher Military Aviation Engineer School (Military Institute), Russia, Irkutsk

NATURE AND PHYSICS OF MAGNETIC STORMS The nature and physical essence of the solar magnetic storms are being developed on the basis of the Sun curl

field nature with its daily rotation.

. ., 2009

106

629.7.036.3

. . , . .

( ), ,

- .

() . - , . - (. - -30). - -30 - 1 000 / . 80 60 .

- - [1]. - [2]:

,

dN N N N Idt

- - = D = (1)

N N ; N - ; DN ; I - ; w = 2pn .

, . - [1], - w - W, - . wS w W :

= + .rr r (2)

. ,

( ) (l = 0) - . - - , , - .

- :

wS = w + W cos l cos b. (3)

. 1.

-

- . - (. 1). 1 2 24 . - 3 1 - 4. 5. - 3 6.

tn0 -

4 2 5

6 3 1

S N

b

,

107

b 0 360. - . 2.

. 2. b -

, - , - . . -, - - ( l), (b).

1. , . . - / . . . . : , 1974.

2. , . . - / . . . . : . . . . -, 1990.

N. V. Danilenko, S. L. Valisevich

Irkutsk Higher Military Aviation Engineer School (Military Institute), Russia, Irkutsk

ROTOR RUNDOWN OF THE GAS TURBINE ENGINE IN THE FIELD OF EARTH ROTATION

The peculiarities of the rotor rundown of the aviation gas turbine engine in the field of Earth diurnal rotation

with account of the plane orientation on the landing field in the horizon plane are considered. Practical recom-mendations to adjust the time of rotor rundown are given.

. ., . ., 2009 669.713.7

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56

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52

50 0 45 90 135 180 225 270 b,

l 52

N

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108

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- .

:

-;

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, - .

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- -, - - .

1. , . . : 2 . . 2 / . . , . . , . . . . : , 1963.

2. , . . : - / . . ; . . . -. . : . ., 1979.

A. A. Zuev, I. D. Zhuk, P. N. Smirnov

Siberian State Aerospace University named after academician M. F. Reshetnev, Russia, Krasnoyarsk

HEAT IN THE LATERAL BOSOM OF COMPRESSION TURBOMACHINES As a result of numerical integration of the system consisting of the movement equation in cylindrical coordi-

nates, the equation of condition and the energy equation, taking into consideration current characteristics under the law of a firm body, current parameters in lateral bosom of compression turbomachines are defined that allows to refuse design procedures of rotary currents with heat which have criterial-empirical character.

. ., . ., . ., 2009

,

109

621.45-181.4:629.78

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- - 8090 . .

:

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:

- (, , - ;

( ); -

; -

. -

, , , - -, . - , . , - -.

L. N. Kajchuk, A. V. Pecarski

JSC Krasnoyarsk machine-building plant, Russia, Krasnoyarsk

M. V. raev


FEATURES OF MODERN CRYOGENIC LIQUID ROCKET ENGINE DEVELOPMENT The possibilities of designing modern engines for space exploration programmes are considered. The new en-

gines are planned to be designed on the basis of liquid rocket engine which have been removed from operational status.

. ., . ., . ., 2009

110

669.713.7

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, - -, - . - - . - - . - , - . , - , , .

,

111

A. A. Kishkin, P. N. Smirnov, S. I. Pshenko


TO THE STATEMENT OF THE PROBLEM OF DISK PUMP INVESTIGATION

Disk pumps, despite low power characteristics, have conclusive advantage on cavitation qualities before wide-

spreading blade pumps. The maximum frequency of rotation also is reached on a shaft of the disk pump. The pumps differ in small noise level, manufacturing simplicity and low cost. Disk pumps are capable to pump over metal and liquid suspensions at their rather small deterioration.

. ., . ., . ., 2009 621.455-181.4:629.78

. .

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-

, . 10. - , z -, w = w2, wx = wy = 0.

- - . w(x) ( )

0,1

( ) 1 21 1

1 1 ,x

v xw ww

-

+ -

(1)

0,55

( ) 1 22 1

1 1 .

v xw

+ -

(2)

w(x) = w1R1/x1 (1) (2) :

0,1

1 21 1

1001 100 .v xx R

w

= +

(3)

(3) , - = 1,21R1, - , 0,1. , (3) .

, - - .

1

* 2.1.2/802.

112

M. V. raev


THE HYDRODYNAMICAL ANALYSIS OF THE BLADE FLOW IN THE OPEN-TYPE IMPELLERS OF THE HYDROMACHINE

The calculated ratios to a hydromachine blade flow are given. The ratios allows evaluating non-continuous

type of the blade flow and the conditions of non-continuous flow.

. ., 2009

621.45-181.4:629.78

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()

10 000 / - -, . , 3 000 10 000 / /V& 107 3 Re > 105. V& , , /V& ( /V& ) = 1106 3, - () [1], .

-

bh

= 3; 2; 1; 0,5 . - -

, - [2]. , - . - - , -

. - , - [3].

- - - . - . - a1 - . - , a1 , . , , -.

- (V& = 01,5 )V& 0,5 3

, - R : / .R RU = -

,

113

-

,R R RU UK = = (1) RK , RK = 0,45.

, , - -. V& , , , . , Dd, - . - .

- - , . - - - - .

- - . - , .

- , [4]. d . , -, . - 1 22 ( )H b a a= + + - 1a , - y = 0 Wu .

Re. - [4]. -, - , . , - .

-

b = c x + a1, (2) . - [4] - ( ) = 0,22 = 0,27.

, - , , - - Wu ( ) Wm ( ) Wn. - [4]:

().uu n

W W fW W

-=

- (3)

, = 0 , -

1

1

,n uaW W

H a=

- (4)

Wu Wu = (U U) = U (1 R- ). (5)

d1 b = bm = 0,5 . W = 0 (2) (3)

d1 = (4,5...4,6). (6)

. . [4] , - ,

d2 = 0,5 , (7) - [3]. -

d = (5,05,1) = K2max H. (8) -

- a1 = a2 = a, (6) (7),

114

222

2

,sin 2

D bK az

- +

(9)

2sin D2; K2 ; K2max = 5,05,1.

-

. 2dt

z=

: 1

1 2

(1 ) . sin

2

z D-=

+ (10)

1 2

1

sin2 .

(1 )z

D

+

=-

(11)

D2

2 12

1 2 2 22 2

2 (1 ) 2 sin sin

2

D Db aKK

-= - + +

(12)

2 1 2

1 22 2 22 2

2(1 ) 2 .

sin sin2

b D D aD KK

- = - +

+

(13)

. - , , - - - - .

- K2 = 4,6.

- . -, -, = d, [4]

1

0,635.2

bb a

+

(14)

, - (12) b2 = 3,48 a1. (a1 = 0,5) b2min = 1,74 . - . , H b2min . - b2 3 (K2 = 4,6) - H 24...25 %. - - . - -, - .

1. , . . - : . / . . ; . . . -. -, 2005.

2. : . . / . . -. . : , 1986.

3. , . . / . . , . . . : , 2009.

4. , . . / . . . . : , 1960.

M. V. raev


CALCULATION AND OPTIMIZATION OF THE WHEELSPACE OF CENTRIFUGAL HIGH REVOLUTION SPEED PUMP

The calculated ratios to construct and optimize the design pump parameters, confirmed experimentally, are

presented. The parameters are calculated on the basis wheelspace of centrifugal high revolution speed pump equipped with open-type impeller.

. ., 2009

,

115

621.45-181.4:629.78

. . , . .

. . , ,

-

, .

- , . . - , Re, - , - D R. D / R, (), , - .

-

2 .

2rwL (1)

- 1 000 / - - . , , .

- - Lr . , Lr , , - 2w ,

2 1 1 ,

2r

rL wCH

= - = - (2)

; - -, (Re; ; ).Df k D=

, (2) , 0,r = - .

9,66 .

l

D

DvK

& (3)

DK = 4 (3)

6 3

min

4,3 10 ,v - =

&

minv 45 10

6 3/. - (N = 1400 ) -

=v& (45300)106 3/, v

&

1,5 107 3.

- [1], , - ( ), - - [2]. - - - , - .

- , ,

v

>&

1,5 107 3.

, , , .

1. , . . - / . . , . . // . . 1 (16). 2008. . 9597.

2. , . . - : - / . . ; . . . -. , 2005.

116

M. V. raev, P. V. Povetkin


ESTIMATION OF CENTRIFUGAL PUMPS SERVICEABILITY Values of design parameters of hydraulic centrifugal pumps are presented on the basis of their hydraulic

characteristics. The practicability to apply open-type impellers of different types is demonstrated.

. ., . ., 2009

532.526; 536.244

. . , . .

( ), ,

,

-

. - . . .

-

- . . - -, , - , - , , -. , , , -.

Nu x - [1]. , Nu x, - . , [2; 3], - . , - [2; 3] - .

, - (), . , , - [1], . - - . - SST .

, , , - , - . -, .

[1] , , :

1* ,gG dK

G g

=t

(1)

G ; ; d ; g .

- (1).

:

,

117

( )0

2opt 1

1

.GG GG

=

(2)

, - . , .

, - , - :

( )01 = + 2 ,

d F

G

(3)

x0 , . - , - .

, - , - , - x0:

( )00

1 0,88ln Re 0,8.

= + (4)

, - . , - [4] W(x). , - (4) -

( )

21,15 .

0,46 ReW

= (5)

1. , . .

/ . . , . . ; . . . , 2001.

2. , . . - / . . -, // . 2000. 6. . 38.

3. , . . - - / . . // . 2005. . 43. 2. . 231248.

4. On the Lambert W function / R M. Corless, G. H. Gonnet, D. E. Hare et. al. // Advances Compu-tational Maths. 1996. Vol. 5. P. 329359.

V. M. Kraev, D. S. Yanyshev

Moscow Aviation Institute (State Technical University), Russia, Moscow

TO THE ANALYSIS AND OPTIMIZATION OF TURBULENT FLOW IN POWER PLANT CHANNELS WITH

TIME-DEPENDENT MASS FLOW The survey of the current state of the problem of hydrodynamically unsteady turbulent flow in channels model-

ing is presented. The optimal form of flow acceleration curve was found. The analytical solution of the Prandtls equation for friction coefficient is given.

. ., . ., 2009

118

621.45-181.4:629.78

. .

. . , ,

*

- - .

-

() - , - ()

21 2 10D

-< ,

1D 2D : 1 1 2 0,1...0,4D D D= = . ,

5Re 1 10w 3

Re 1 10 , Re .

() , , 3 ( 22 =b ) - 7...5,31 =b . - - :

( )( )

2 2 2 21

2 1 2 2 1

sin2...10.

sinm

m

b D zFWF b D z

-= = =

- (1)

,W , ,

( 1 30 , ( ) ,b i w ie = e + e - e g

P ; a, w, r, i , , - ; b , - ( ). - - [2].

- ( - ) 1,4 5 [1] - Wt, - WP:

= 0,57 WP + 0,481, Wt = 0,49 WP + 0,165. WP, , [1] S C :

WP = 0,067 74 0,000 64 S + 0,004 78 C. [1]

t = + W 2,

'' (1), W2 , ; , . 5 - , 1,4 = 0,532C, - [1].

1

* - 09-05-91061.

188

. . [2]. - 11 , 0 76 %, . - 0,045 26,5 . - [3] . - 76 54 %.

-, - - 0,3 14 , - 5 14 , 34 %. ,

, 1,7 0,6 . - .

1. Wang, J. R. An Empirical Model for the Complex Dielectric Permittivity of Soils as a Function of Water Content / J. R. Wang, T. J. Schmugge // IEEE Trans. Geosci. Remote Sens. 1980. Vol. GE-18. . 4. P. 288295.

2. Stogryn, A. Evaluation for calculating the di-electric constant of saline water / A. Stogryn // IEEE Trans. Microwave Theory Tech. 1971. Vol. MTT-19. P. 733736.

3. Curtis, J. O. Effect of Soil Composition on Dielectric Properties / J. O. Curtis, C. A. Jr. Weiss, J. B. Everett // Technical Report EL-95-34. Decem-ber, 1995.

p, p, [1], [2] m, m.: a 0,3; 0,5; 1,4; 5,0; 10 14 ; 5,0; 10 14 . , ;

: 'm = 0,46 + 1,06'p , "m = 0,08 + 1,01"p

V. L. Mironov, A. Yu. Anisimova


S. V. Fomin, L. G. Kosolapova

L. V. Kirensky Institute of Physics, Russian cademy of Science, Siberian Branch, Russia, Krasnoyarsk

DOMAIN OF APPLICABILITY STUDIES FOR SCHMUGGES

DIELECTRIC MODEL FOR MOIST SOILS The domain of applicability and error of well known in radar and radiometer remote sensing Schmugge

dielectric model for moist soils have been investigated. The model examination have been provided on the comprehensive dielectric data set for different soil types, wide frequency range and the moistures up to field capacity values obtained by Curtis.

. ., . ., . ., . ., 2009

189

528.8

. .

. . , , ,

* ,

NOAA-AVHRR Terra-MODIS. - .

: -

, NOAA, Terra - = 1: 500 000 -, , , ;

;

- = 1:500 000;

- 1,5 JPG;

; -

. -

- , - ftp://data:[email protected]/DailyData/.

, , - () NOAA/AVHRR Terra/MODIS - - 19962009 . - - Current & Archived Significant Global Fire Events and Fire Season Summaries, - http://www.ruf.uni-freiburg.de/fireglobe/current /globalfire.htm.

, - - - . - -, -

2 200 . - BIRD/DLR Transparent World FIRE. - , , - .

- N/AVHRR/TOVS, - . - 1,6 , NOAA 16-19.

- . - N/AVHRR/TOVS - , 5- - 30 %, - - .

N/AVHRR - - .

(NOAA) (Landsat-ETM) -, , , 27 % 1 000 16 % 5 000 , - NOAA - .

2

* ( 09-05-98008-__).

190

-, , . - -.

- - , - 2002 . - 5 . - . , , , 0,7 2 - , . - 2 . . NOAA, TOMS - 2, , 4, - - 2002 . -

( 5,4 , ), 1,5 , 0,8 , 70 .

- - ( - ), -. - - , .

, (1998), (19972002), -, (2002), , , - , - (2003, 20072008), -, .

, - - .

A. I. Sukhinin

V. N. Sukachev Institute of Forest, Russian cademy of Science, Siberian Branch, Russia, Krasnoyarsk

AEROSPACE MONITORING OF CATASTROPHIC

WILDFIRES IN EAST SIBERIA The probability approach of wildfire detection, energy release and fire scars estimation is developed using

NOAA /AVHRR and Terra/MODIS information. Catastrophic wildfires in East Siberia behavior is discussed. We can conclude that the mechanism of fire propagation by irradiative flux is dominant for high intensity surface and crown fires.

We propose the hypothesis of positive feedback between anticyclone growth and energy release from wildfires for the huge burned territories. The critical number of fires is defined when the fire situation becomes uncontrolled according to the total fire intensity.

. ., 2009

191

528.873

. . , . . , . .

. . , ,

. .

- , , -

2006

2006 .

, -

, - , - -, . -, - . - - -, - . - .

, , - , . - 2006 ., - - 59 52 . ., 101 33' . .

, - [1]. - - - - - , - - -. - , , - , - AVHRR NOAA, -

MODIS/Terra. -. , , -. , - . AVHRR/NOAA - , , , 30 %.

9 2006 . 31 2006 . , , 17 936,53 .

-, , - 120 /, - 40 %. - - , [2], 316 000 .

, 45 % , (. ).

192

- / [3], -

1. , . . / . . , . . , . . - // . 2008. . 1(18).

2. Wooster, M. J. Retrieval of biomass combustion rates and totals from fire radiative power observations: FRP derivation and calibration relationships between biomass consumption and fire radiative energy release / M. J. Wooster, G. Roberts, G. L. W. Perry, Y. J. Kaufman // J. of Geophys. Research. 2005. Vol. 110.

3. Soja, A. J. Estimating fire emissions and disparities in boreal Siberia (1998 through 2002) / A. J. Soja [et al.] // J. of Geophys. Reseach. 2004. Vol. 109.

N. V. Trofimova, E. G. Shwetsov, A. I. Sukhinin


A. V. Ivanov

Saint-Petersburg State University of Information Technologies, Mechanics and Optics, Russia, Saint Petersburg

DAILY AVERAGE DYNAMICS OF SMOKE EMISSION ON AN EXAMPLE

OF SINGULAR FIRE IN 2006

The daily average estimation of a mass exit of fire emission on an example of singular fire in 2006 is given.

. ., . ., . ., . ., 2009

528.88.042.4:630

. .

. . , ,

MODIS. - . .

- . , MODIS, Terra Aqua, , - [1].

, , - , - [2]. -, , - .

, - , -, ,

, [3]. , - - [4]. - , - , .

- , - , - 2006 . - MODIS. -

193

- , - MODIS. - , , 0,95.

- , 21 MODIS, [3; 5].

FRP = 4,341019(T48 T4b8), (1)

FRP (/); T4 T4b , - MODIS.

- - 12 4 396 . 551 . , - , . , , 200 , 43 % .

, . -, , , - , [5]. - - . , [6]:

Rbiomass = 0,368(0,015)FRP, (2)

Rbiomass (/); FRP ().

, -, 6 200 - , 2 .

, - . - - [7].

1. Justice, C. O. The MODIS fire products / C. O. Justice [et. al.] // Remote Sensing of Environ-ment. 2002. Vol. 83.

2. Wooster, M. J. Fire radiative energy for quan-titative study of biomass burning: derivation from the BIRD experimental satellite and comparison to MODIS fire products / M. J. Wooster, B. Zhukov, D. Oertel // Remote Sensing of Environment. 2003. Vol. 86.

3. Kaufman, Y. Relationship between remotely sensed fire intensity and rate of emission of smoke: SCAR-C experiment / Y. Kaufman [et. al.] // Global biomass burning. J. Levine (d.). MA : MIT Press, 1996.

4. Wooster, M. J. Small-scale experimental test-ing of fire radiative energy for quantifying mass combusted in natural vegetation fires / M. J. Wooster // Geophys. Research Letters. 2002. Vol. 29 (21).

5. Kaufman, Y. J. MODIS ATBD: Fire Products (Version 2.2, Nov. 10, 1998) / Y. J. Kaufman, C. O. Justice // EOS ID#2741. 1998.

6. Retrieval of biomass combustion rates and to-tals from fire radiative power observations: FRP derivation and calibration relationships between bio-mass consumption and fire radiative energy release / M. J. Wooster, G. Roberts, G. L. W. Perry, Y. J. Kauf-man // J. of Geophys. Research. 2005. Vol. 110.

7. Dozier, J. A method for satellite identification of surface temperature fields of sub-pixel resolution / J. Dozier // Remote Sensing of Environment. 1981. Vol. 11.

E. G. Shvetsov


ESTIMATION OF FOREST FIRE ENERGY PARAMETERS

USING SATELLITE DATA

Estimation of forest fire energy parameters using MODIS data is performed. The total biomass consumption values are calculated using fire radioactive energy measurements. Fire front line intensity is evaluated using sat-ellite data.

. ., 2009

194

550.837

. .

. . , ,

. .

. . , ,

. .

. . , ,

-

. 10 %.

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, - - , - , () - () [1]. - , - () , - [2]. - .

- - - (. 1). a = 0,002 L = 0,12 , (x = 0, y = 0, z = D).

V(t), , T. , ,

(x = 0, y = DL, z = D). - () - , - - [1]. - [3].

T1 = 3,0 T2 = 0,3 , . - , , DL t, - (. 2).

. 2. :

1 ; 2 T = 1,5 , 3 T = 0,1 ; 4

T = 3,0 ; 5 T = 0,3 ; 6 T = 0,2 1

-

DL, - (. . 2).

. 1.

195

[1] [2] -, [4] .

. 3. Dm D

: 1 = 3,0 , s = 6,6102; 2 = 0,3 ,

s = 1,3102; 3

, , - [4, . 19], , , . - 1 (. . 2), - , , V(L) L

(0)

( )

1( ) ( )( ) (0)

f

f L

V L V f dff L f

=- , (1)

V(f) , 1; f(L) , -

, - L = (4D DL)1/2; f(0) , - . , - t , - , (1), L, - ( ) Dm .

(. 3), , , - , - - 10 %.

1. -

/ . . , . . , . . -, . . // -. 2007. . 48. 12.

2. - / . . , . . , . . , . . // . 2009. . 50. 2.

3. Pulse Electromagnetic Sounding of the Petro-leum-Containing Layered Medium / M. I. Ehpov, S. A. Komarov, V. L. Mironov, K. V. Muzalevsky // Proc. IEEE Geosci. and Remote Sens. Symp. Barce-lona. 2007. Vol. VII.

4. , . . - / . . . : - . ., 1975.

M. I. Epov

A. A. Trofimuk Institute of Petroleum Geology and Geophysics, Russia, Novosibirsk

V. L. Mironov


K. V. Muzalevsky


METHOD TO DETECT THE WATER-OIL CONTACT IN OIL-SATURATED RESERVOIR BY UWB PULSES

The detection method of the water-oil contact of oil saturated reservoir in the logging process is proposed by

the pulses of nanosecond duration. The distance from antenna to water-oil contact to be estimated with an error in order of 10% is demonstrated.

. ., . ., . ., 2009

196

911.2; 631.58; 631.4; 528.93

. .

- , ,

. .

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( ) -- . - () : , , , (), .

--

- - - (). - .

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- . - (), , , - . - - , .

- - - () . (); ; - ; - ; -

- ; - , , ; ( ) ; (-) - ; - - .

- , -, - - - (). - - , - , - - - /GPS.

, ; , - ; - /GPS - .

- () - - -

197

(-) .

, , - .

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() : - - ; - - -, -, - -- .

- -- 5 .

- - (30...100 ) ()- () -

- . - 15 51 . - - , , - , - - .

- -, - . 9 -. .

- () - - - - , NDV - - - .

S. E. Perfil'ev

Krasnoyarsk Research Institute of Agriculture, Russian cademy of Science, Siberian Branch, Russia, Krasnoyarsk

A. K. Cherkashin

V. B. Sochava Institute of Geography, Russian cademy of Science, Siberian Branch, Russia, Irkutsk

APPROACHES AND PRINCIPLES OF MAPPING AGRARIAN LANDSCAPES

OF THE SOUTH OF THE CENTRAL SIBERIA Approaches and principles of mapping agrarian landscape the south of the Central Siberia (Krasnoyarsk re-

gion) for the organization space the agrarian industry monitoring are considered. On Space pictures the average sanction the base circuit of the spatial organization of geosystems is submitted by way of ranks (agro) landscape structure: the country; area; a province; the district (landscape), connected to administrative areas.

. ., , . ., 2009

198

- .pdf

-

237

669.713.7

. . , . .

. . , ,

-.

. - - , -, - -. - , , . , , -, , . , , . - - , - . - , - . - , - - , , -. , .

, - - . (). 180 196 , -

. , 170 . , - . , - . , , (. ). , 0,8 103 170 . , - . 170 196 , - , - ( 107 165 ).

, 0 0,2 0,4 0,6 0,8 1 1,2 1,5 2

, 78 88 95 99 103 106 108 112 117

-

: - , -, - , , . - - . . , , , - [1]:

238

,

pdmd RT

W = (1)

W - ; ,p T ; m ; ; R .

- :

0 0 ,

q F pdT rd mc mcRT

W= - (2)

r ; .

- , , - :

1 ,dh dm d dhvd d d dv

r = - t r t t (3)

v ; h ; .

- .

- , - .

1. , . . - / . . . . : , 1984.

N. V. Baturov, Yu. A. Filippov


PERFECTION OF CRYOGENIC TEST TECHNOLOGY OF FLYING MACHINE NODES

Cryogenic test technological parameters of pneumohydraulic node systems and automatics for the purpose of

perfection and increase of working capacity of aircraft products are considered.

. ., . ., 2009

620.178.154.56

. . , . . , . . , . .

. . , ,

-

.

, -, - - - , - , - , - , -.

- () -

, , . -, - , .

- -

-

239

- (). , , , - . - - 20,8 10- ( 56 10- . . .) 150 110 - . - . - . - - - . - - - . , - , -, - - - -.

- - , ( - ). -- - , - - . - , - . , - .

- , . - , - - , - . - - , .

S. S. Bezrukih, N. P. Sedlov, E. N. Golovenkin, A. A. Kuptsov

JSC Academician M. F. Reshetnev Information Satellite Systems, Russia, Zheleznogorsk

PROBLEMS OF CARRYING OUT THERMOVACUUM AND THERMOBALANCING TESTS OF SPACE VEHICLES

OF PARTIAL-PRESSURE SYSTEM OF THERMOREGULATION ON THE BASIS OF THERMAL PIPES

The necessity to create the newest complex for carrying out thermobalancing and thermovacuum tests of par-

tial-pressure satellite is presented.

. ., . ., . ., . ., 2009

240

629.783.05:681.3

. . , . . , . .

. . , ,

-

. -

( ), , , - , . , - - 1015 . - - () MS-196, -, . , , .

-, -- - (), [1].

- -, :

- , ;

- ;

;

;

- ;

.

-- . - , - -. , (- , . .), , - ROBO-4000.

- - . - -, , - - .

1. , . . - - / . . // : XII -. . . ; . . . -. , 2008. . 152153.

E. A. Klyuev, V. V. Furmanov, V. N. Shkolny


ABOUT RESULTS OF CARRYING OUT STANDALONE TESTS OF CONTROL BLOCKS OF THE ONBOARD CONTROL COMPLEX

USING LABORATORY WORKING OFF COMPLEX Results of application of created laboratory working off complex are described in the period of carrying out

standalone tests of the developed instruments.

. ., . ., . ., 2009

-

241

621.3.08

. . , . . , . .

. . , ,

, -

, , , -, -. , - .

,

- , - , . , - , - . ( -, -) - (, -, ) - - ().

- , , , , , (). - - -, .

, , , - , , - . -

( ) ( )1 1

1 1 ,n m

i jN n m n i m j

= == + - + + - +

N ; m ; n - .

, , , . 1, - -, - , N = 137.

-

- , 5 .

1 , 7 . - .

-- - , - -,

. 1.

.

// 1

// 2

// 3

// 4

// 5

// 6

// 7

// 8

.

1

2

3

4

5

6

7

//

//

//

//

//

//

//

242

(), - - -. - . 2.

RS-232C USB-2.0,

-, , , - , - .

-1.0 - :

- - 10 , 50 100 ;

- -;

, ;

- , - -; - , -; ; - .

- - .

A. V. Pechatkin, M. S. Anufrik, O. A. Zelentsova

Rybinsk State Air Technological Academy P. A. Solovjeva's name, Russia, Rybinsk

TEST AUTOMATION OF CORDLIKE JUNCTIONS FOR SPACE EQUIPMENT

Complexity of modern on-board electronic equipment of space vehicles results in necessity of increase of

quantity of units and modules and, as consequence, to increase and complication of cordlike junctions which pro-duction quality directly influences performance of airborne equipment. Thus, boosting of efficiency of the bundle supervision is the important and extremely actual problem.

. ., . ., . ., 2009

533

. . , . .

, ,

-

- .

- - - .

- - . -, - (70 ),

. 2.

-

243

-.

. , , , - .

- - , , -- .

- - , - , - , - - : , , - , .

- - , 4 3 /.

- ICP CON, - 8 , . 10 .

3 1 / ( ) - 60 . - 110 , , - - - .

- - -, -. , Flow Simulation 2009. - , - .

A. V. Svistunov, A. A. Sitnikov

The Ufa State Aviation Technical University, Russia, Ufa

VORTICAL SYSTEM OF CLIMATIC TESTS OF SPACE-ROCKET EQUIPMENT The actual problem of developing and carrying out ecologically safe climatic tests of space-rocket equipment

is considered.

. ., . ., 2009

621.4

. . , . .

, ,

-

. , , - .

-

, - - (), [1]:

, -;

-,

244

, ;

- , ;

, . . .

- - -:

2 2

1

1 ;1

n

ii

dmw df kdw dQM f m a =

-= - - -

(1)

( )( ) 2

2 21

1 1;

1

n

ii

k kMTdT dQ XM a =

- - = +

- (2)

22 2

1

( 1)1

n

ii

p k kdp M dQ YM a =

- = + - , (3)

( ) ( )2 21 1dm dfX k M k Mm f

= - - - ;

2 2dm dfY kM kMm f

= - .

, - [2]. - , - , - , - .

- .

. - , [3]. - :

( ) ( ) ( ) ( ) ( )22, , 1 ;

T R T Rc T T R T

R R R

= (4)

( )0 , 0;R s< < > ( ) ( )( )0,0 , 0; 0 ;T R T R s= (5)

( )( )

( ) w , 0;ir mTT T T

R FR s

- = - - >

= t (6)

0, 0,0

TR R

= >

= (7)

- .

100 - - (4)(7). .

1. , . . - / . . , . . // - : . . . ; . . . . -. , 2002. . 184188.

2. , . . / . . . . : , 1963.

3. , . . - / . . . . : , 2005.

N. M. Cirelman, R. R. Mustafin

Ufa State Aviation Technical University, Russia, Ufa

MODELING HEAT-MASS EXCHANGE PROCESSES AT HYDROCLEARING OF SOLID-PROPELLANT ROCKET ENGINE

Liquid drops and gas flow heat-mass exchange processes mathematical model and applicable PC calculations

operation algorithm are given. A model problem of water drops being evaporated during their injection into the SRM input is to be resolved, taking into account gasflow cross section shaded by the drops and the present drop radial temperature gradient.

. ., . ., 2009

.pdf

51

621.396:531.395

. . , . . , . . , . . , . . , . . , . . , . . , . .

. . , ,

-

. - , .

() -

- , Anik-F2, Thaicom-4 . - - , (). - , - . . - . , . - .

(-) - 5 . , . - , . - , , - , . , - , , .

, , - -

, , . - - . -. , - - 1 600 .

- - . - . .

, , - , ; - ; - - .

- . - (, , ) .

- - , - ,

52

, . - - . - , - - , - - - . - .

- -, . - (), ()

. - - - . - : - - - .

MSC.Patran-Nastran .

. - -/0.1 ( 2800688) 1-596-36-98 0,110,13 . : 8,5 ; 2,5 .

K. P. Baslyk, N. A. Bey, V. A. Vechtomov, V. N. Zimin, B. L. Kogan, A. V. Krylov,

V. E. Meshkovsky, A. A. Smerdov, S. A. Churilin

Bauman Moscow State Technical University, Russia, Moscow

IMPLEMENTATION FEATURES OF DEPLOYABLE MULTIBEAM AEROSPACE ANTENNA

The release of Russian multibeam aerospace antenna for satellite communication system of geostationary

spacecraft is under consideration. The results of mirror surface numerical optimization and analysis for main strength parameters of multibeam antenna module under launching dynamic forces are presented.

. ., . ., . ., . ., . ., . ., . ., . ., . ., 2009

539.3

. . , . .

- , ,

. .

. . , ,

-

, . -

, - - . -

53

- . - , - , . - - , - - .

-- - - . - - - - - . - [1], ANSYS (. 1). ( ) ARISE, LGarde, Inc [2].

. 1. - 3D-

,

. , - - - , - . , - (. 2).

, - [3], .

. 2.

- , . - , - ( 50 140 ), - - 35 . - - 3,5 , . . . , .

1. , . / . ; . . . . . : , 1975.

2. Greschik, G. Torus-less inflated membrane re-flector with an exact parabolic center / G. Greschik, M. M. Mikulas, A. Palisoc // AIAA. 2004. Vol. 42, 12. . 25792584.

3. , . . / . . , . . // : . . . . . . . 1. : - , 2003. . 2223.

54

A. V. Belkov, S. V. Ponomarev

Research Institute of Applied Mathematics and Mechanics of Tomsk State University, Russia, Tomsk

A. I. Velichko


QUESTIONS OF MODELLING THE INFLATABLE REFLECTOR

The technique of computer modelling the inflatable reflector of a space vehicle, based on the mechanics of the deformed firm body, is considered.

. ., . ., . ., 2009

629.78

. .

. . , ,

-.

. - - -.

() - 25- . , - , , - .

- . . - ( ), 1964 . - - , -, ,

- , .

, - , - -. . , - , . . - - - , .

, - . - -3, - 2009 .

- 2009 . Iridium-33 - -2251.

55

Yu. L. Bulynin


ANALYSIS OF MEETING REQUIREMENTS OF THE INTERAGENCY COORDINATE ON SPACE DEBRIS PREVENTION

The requirements of interagency document Directive principles of work organization to lower space debris

mitigation are considered, the necessity of their implementation is discussed.

. ., 2009

539.3

. . , . . , . . , . . , . .

, ,

. .

. . , ,

-

-

. -

- [1]. - . .

- - , - - - [1; 2].

- - . , , , . - , . , - , - .

, E, E.

- , . - - 6 - . - - , , , .

1. , . . - / . . -, . . , . . // . . 15. 2007. . 1(146).

2. , . . / . . // . . 15. 2007. . 2(147).

56

. V. Gerasimov, . P. Zhukov, S. N. Kulkov, S. V. Ponomarev, Yu. F. Hristenko

Tomsk State University, Russia, Tomsk

V. I. Halimanovich


THE SIMULATION OF STRESS-STRAIN PROPERTIES OF THE CARBON-FILLED ROD STRUCTURE ELEMENTS

The stress-strain properties of the carbon-filled rod structure are considered. The damages generated by ex-

ternal actions are taken into account.

. ., . ., . ., . ., . ., . ., 2009

629.76/78.023

. . , . .

. . , ,

. -

- , . - - . - .

- - . - - , . . - , - , - - , , -, . , -, , , -.

- - , , , - . - - . - 2- . . 0,5 2. - - , . - 2- - - . - - - . - 54.497 - . - , -

57

.

, . - .

(. 1) - , .

. 1

(. 2) - , - .

. 2

-

. - -, , - (, ).

V. V. Dvirnyi, V. P. Vashkevich


QUALITY ASSURANCE PERFECTION OF NON-GLUED ITEMS

The comparative analysis of various methods of non-destroying quality assurance is conducted.

. ., . ., 2009

539.3:621.396.67

. . , . . , . .

- , ,

. . , . . , . .

. . , ,

-

, . -

, , - -

. , - , .

. . . . -

58

[1]. - . - [2]. - - , - , - [3; 4] . - - [57]. . - - ().

- - - . - . , - - () -.

- . - - . - - -- . [8], ANSYS. -

. c - FEKO GRASP [9].

- - - , - , .

1. , . . / . . , . . -. . : , 1987.

2. Tibert, G. A. Deployable Tensegrity Structures for Space Applications : PhD thesis / G. A. Tibert. Stockholm, 2002.

3. , . . -- - : . ... . -. / . . . , 2006.

4. , . . / . . , . . , . . , . . // : . 2004. 10. . 1018.

5. , . - / . , . // - . 1991. 1. . 6169.

6. Agrawal, P. K. Preliminary design of large re-flectors with flat facets / P. K. Agrawal, M. S. Ander-son, M. F. Card // IEEE Transactions on Antennas and Propagation AP-29. 1981. 4. P. 688694.

7. Lai, C.-Y. Analysis and design of a deployable membrane reflector : PhD thesis / C.-Y. Lai ; Univer-sity of Cambridge. USA, 2001.

8. , . / . ; . . . . . : , 1975.

9. Pontoppidan, K. GRASP: Technical descrip-tion / K. Pontoppidan. Ticra, 2005.

A. S. Evdokimov, S. V. Ponomarev, Yu. I. Buyanov


A. V. Romanenko, D. B. Usmanov, G. V. Shipilov


THE CONNECTED MECHANIC AND ELECTRODYNAMIC ANALYSIS OF TRANSFORMED SPACE REFLECTORS

The variant of a complex technique of computer modelling of the transformed spacecraft reflectors, allowing

to reach the best antenna characteristics, is considered.

. ., . ., . ., . ., . ., . ., 2009

59

629.78.023

. . , . . , . .

. . , , -

, -

, .

()

:

() 10 00015 000 ;

;

- .

- , - , - .

- (), . 1989 . - 78 , . - - . - , . ~ 17 , - 8 .

() (. ) ( ) 1; 2; ( , ) 3; 4; - 5; 6. .

25 . : 0,4 , 0,3 .

, - - :

- ;

- ( 2 /);

- ;

.

1 3 - (), - , -- . - - .

, . - , .

, - , . . .

- , ( -), , - . 2,53 .

60

M. I. Kislitsky, V. A. Cherepanov, V. V. Golovanova

FSUE Design Engineering Bureau Arsenal named after M. V. Frunze, Russia, Saint Petersburg

CONSTRUCTING A STANDARDIZED MODULARIZED SMALL UPPER STAGE TOR ON THE BASIS

OF SOLID-GRAIN ROCKET ENGINE

The main idea of project Tor consists of constructing a standardized small upper stage on the basis of the solid-grain rocket engine produced in lots constructed by FSUE Design Engineering Bureau Arsenal.

. ., . ., . ., 2009

629.78.023

. . , . .

. . , ,

, , .

. , , ,

, . . - , :

() ;

- (, , ), - -, , ;

, , , . .

, , , -, .

. , -. (, , , .) , .

, , , , . - - . - , - -, -.

, , - , - - :

- -, -;

, - -;

;

.

61

, . , -, , , , - , - .

, - , .

, .

1. . - , , - , . 10 . , , - (

) - ( ). , .

2. , - , , .

3. - , , , .

4. - ( -) . , , -, .

, - - .

A. A. Kopchegashev, V. V. Dvirnyi


IMPROVING SOLAR BATTERY SKELETON ASSEMBLAGE OF COMMUNICATION, NAVIGATION AND GEODESY SATELLITES

The technique to improve quality and productivity of solar battery skeleton assemblage are introduced. Advan-

tages of case knot laser processing are shown.

. ., . ., 2009

62

331.015.12:629.78

. .

. . , ,

. .

. . , ,

-

, . . , - . , - , , . .

- (), - . . ( ) ( 2008 . ), - 1 000 . - - - - . , - SESAT () 10 , 9 ; - - 12 . 20082009 . -5 (), 300 () . . 15 . - , - .

- () , , . - , - - , , - - . -

, -. - , (, , - , ) - .

, 90- - - - . , -, , - - - . - (- ), .

15 , 30 , , , , , , - . - 2028 . - - , . , - ( ) 60 %

63

, . , 50 % - . - - . -, - - , - - - .

, , - - - , - : , [1].

- , - - , [2], - [3], [4]. , - ,

; , , - .

.

1. , . . : / . . ; . , 2008.

2. , . . - : . ... . . / . . ; . -26, 1979.

3. , . . - - : . . - . / . . ; . . -. -. , 2005.

4. , . . - - : . . - . / . . ; . . -. -. , 2007.

S. G. Kochura


A. A. Nosenkov


ABOUT TECHNOLOGICAL LEVEL OF AUTOMATIC SPACECRAFT ELECTRICAL TESTS PROCESS

The paper deals with the problems of technological level ensuring by quality and effectiveness criteria in

electrical tests process of the automatic spacecrafts, produced by JSC ISS named after academic M.F. Reshet-nev. It is shown that this field of scientific and technical knowledge, in spite of the reached progress, is very im-portant for further investigations. Problematical tasks and proposals for their solutions are formed.

. ., . ., 2009

64

669.713.7

. .

. . , ,

-

. ()

- (), - . . - , - - . -, , , - , , -. - - . - - .

- , , , , - , . . -

, , - . - - , - - , , , , - . - -, .

- - EULER. - . - , , , - , , , EULER, - . , - .

A. V. Krylov


SIMULATION OF DEPLOYMENT MULTIJOINT SOLAR ARRAY AT GROUND TESTS

The application of mathematical modeling of the deployment transformable structures during their working off the ground is considered.

. ., 2009

65

677-486.2:539.11

. . , . . , . . , . .

. . , ,

. .

. . , ,

, , - . - . .

-

() . - - . - , - - . , MATLAB. - - , , . , :

1. , - , - . - .

2. -, , - , - - , . , . - .

L. . Kudryavin, O. F. Belyaev, V. . Zavaruev, . S. Kotovich

Moscow State Textile University named after A. N. Kosygin, Russia, Moscow

S. F. Podshivalov


CALCULATING THE METAL KNIT 2-D DISTORTION BY NONLINEAR ELASTICITY THEORY

The paper is devoted to description and application of metal knit 2-D distortion, produced by nonlinear elas-

ticity theory. The metal knit is used as echoing area of space antenna. The examples of the programme application to calculate the distortion of several types of the knit are presented. The calculation results perfectly coinsides with the experimental ones.

. ., . ., . ., . ., . ., 2009

66

629.7.01

. . , . .

- - -, ,

-

. . .

() - (), - (- , - ). - - - (). - - , - . - .

- . - - . -, , - , , , .

- , , - , - - - .

- :

; ,

; -

, - ( - ) .

. - . - . - , - . - , .

- .

67

V. I. Kurenkov, V. V. Lokhmatkin

State Research-and-Production Space-Rocket Center TsSKB-Progress, Russia, Samara

THE EFFECT OF ONBOARD SYSTEM RELIABILITY INDEX UPON SPACECRAFT OUTPUT EFFECT

The paper deals with the space observation system goal efficiency effect of partial spacecraft onboard systems

failures. Dependence of spacecraft reliability index effect upon sensing satellite output effect is derived on the basis of mathematical failure model. Simulation algorithm is derived for the space observation system efficiency prediction.

. ., . ., 2009

629.78:621.8

. . , . . , . .

. . , ,

. . , . .

, ,

-

-

- .

, -

-- , - , - (), - () .

, - .

, , - , , .

- , . - , - (), -- - ( , -

, .). , -- - .

- , -, - , - - . - , , - , -, . - .

, , - -, , - . -

68

, , - , , , - - .

, - -, - , x. x1 x2 - , , , - , - .

-, . - . , , - .

. - - -. , .

- - , , - , , - , - .

- - , .

, - - - .

A. V. Lekanov, A. B. Gurylev, D. A. Cherepanov


P. N. Silchenko, E. S. Novikov

Siberian Federal University, Russia, Krasnoyarsk

SOME CONTROL OPPORTUNITIES OF FUNCTIONAL-OPERATIONAL PARAMETERS OF DRIVE TOOTH GEARINGS OF SPACECRAFT

EXECUTIVE AUTOMATICS AT A DESIGN STAGE The methods to maintain the required functional-operational parameters of drive tooth gearings of

spacecraft executive automatics are considered at reduced weight and mass parameters.

. ., . ., . ., . ., . ., 2009

69

539.3

. . , . . , . .

- , ,

-

. -

- -. - , , , - ( ).

, - (, ) , , - .

- - - . , , -, -

-, . ( - 163763 . . ).

- - .

- . - [1] -.

1. , . : . / . -. . : , 1987.

S. V. Ponomarev, A. P. Zhukov, M. S. Pavlov


SUBSTANTIATION OF A MECHANICAL METHOD TO DEFINE

AN INTENSE CONDITION OF TRANSFORMED REFLECTOR ELEMENTS The problems of a theoretical and experimental substantiation of a method to define the intensity by local de-

formation elements and a reflector echoing area are considered.

. ., . ., . ., 2009

70

629.78

. . , . . , . .

- , ,

. .

- - , ,

,

.

- . -, , - . - , - -, . - - - - . . - , - 20 % .

. 16026018 - . - 56 .

26046018 . - () 32 .

() :

Q = t, P , -, ; t .

- :

0,5 ; 0,05, 0,1 0,2 ;

17 ; -

; -

;

95; -

-31.

. , - 200 (. 1, 2).

. 1. - , 0,05 ,

200

. 2. - , 0,2 ,

200

, 26046018 100 300 .

71

16026018 20 200 . .

(. 1. 2) , - - . 0,05 , - - , - , . , . 2,

- .

0,05 .

- 26046018 34 13 100 300 .

16026018 42 5 20 200 .

O. G. Rassolov, K. A. Goncharov, V. A. Antonov

Co Ltd. Scientific Industrial Enterprise Thermal Generating Units and Systems, Russia, Khimki

V. A. Alekseev

FSUE Research Institute of Precision Instruments, Russia, Moscow

HONEYCOMB SUPPLIED WITH HEAT TRANSFER TUBE AND HEAT-RETAINING MATERIAL

Honeycombs supplied with heat transfer tube are the power construction elements of a spacecraft. At the same

time these honecomb constructions are heattransferring devices, able to protect the surface equipment from the excessive heat.

. ., . ., . ., . ., 2009

539.3

. . , . .

. . , ,

. -

. -

- . -, - . - . - . - .

- .

[13]. - , - (. 1).

. 1.

72

- .

-

, . - , - . . 2. .

.

- - .

1. , . . - - / . . , . . // . . 1(14). 2007. . 47.

2. Pellegrino, S. Deployable membrane reflectors / S. Pellegrino // In Proc. 2nd World Engineering Congress (2225 July 2002, Sarawak). . 19.

3. Akira, M. In-orbit deployment performance of large satellite antennas / M. Akira // J. Spacecraft and Rockets. 1996. Vol. 33, 2. . 222227.

M. A. Rutkovskaya, A. V. Tarasenko


MODELING THE TELESCOPIC COMPOSITE SPOKE OF THE BIG SPACE ANTENNA

The problem of extension of the telescopic spoke is solved. The geometry optimization is realized and their in-

fluence on frequencies of the spoke is defined.

. ., . ., 2009

541.64:535.135:541.136

. . , . .

- , , ,

. .

- , , ,

. .

. . , ,

-

, - . : - , , .

-

(), - , - , - ,

- .

- - .

. 2.

73

, - , .

, - -, -.

, ( - ). - .

- ( ) ( - ) -.

- , - - .

, - - -, 100 %.

- , - .

, .

: , - -, , .

- -:

, -

-

- n

525 215 2,4 -4 420 240 1,8 615 192 3,1 5-211 436 187 2,3 -200 560 280 2,0 -69 553 430 1,2

- . , -4 -11 6,6 , - 4,2 -, 6,8 %.

, - - - , -- ( - ) , - .

-- , . . . - , .

V. I. Slivinsky, . . Karpikova

Ukrainian Research Institute of Engineering Technique JSC, Ukraine, Dnipropetrovsk

N. . Verbitskaya

Scientific and Production Firm Plastik LLC, Russia, Saratov

V. . Gajdachuk

N. E. Zhukovsky National Aerospace University Kharkov Aviation Institute, Ukraine, Kharkov

CREATION OF ENERGY-SAVING TECHNOLOGIES OF FORMING ARTICLES MADE OF POLYMERIC COMPOSITE MATERIALS WITH THE RAISED

MECHANICAL CHARACTERISTICS The concept of creation of power to save up manufacturing techniques of the polymeric composite materials is

stated. It allows to reduce a cycle of heat treatment and raise mechanical characteristics of a material.

74

The concept is based on obtaining of the pattern of changes occurred in physical state of the polymer: the polymer reaching the minimum viscosity, gel formation start, highly elastic and glass-like state and completion of curing process.

. ., . ., . ., . ., 2009

620.22419.8

. .

. . , ,

-

, . - .

-

- - . - , , - . - - . - , , - [1]. - - - .

- , [13]. - - -.

, - Y, - - - :

( )( )

, ,

, ,

U x y z dxdydz

U x y z dxdydz

DY =

%

% ,

( ), ,U x y z% - ; ( ), ,U x y zD % .

- [1]. - - , [2]. - : , [3].

( . ) .

- , [2].

75

( , )

-

-- - : -, - - .

, - - -

- .

1. Zinoviev, P. A. Energy Dissipation in Com-posite Materials / P. A. Zinoviev, Y. N. Ermakov. Lancaster : Technomic Publishing Co., 1994.

2. , . . - - - : . . . / . . . ., 2007.

3. . . / . . // -. 2006. 2. . 1218.

. . Smerdov


POSSIBILITIES OF DAMPING CHARACTERISTICS CONTROL FOR COMPOSITE ELEMENTS OF LARGE-SIZE

SPACE TRUSS STRUCTURES Possibilities of damping characteristics control for composite elements of large-size space truss structures,

which appear at the choice of optimal reinforcement structure, are studied. At the example of carbon fiber plastic bars for reflector of space vehicle Condor-E the compromise optimization possibilities of composite elements' dynamic and dissipative characteristics are showed.

. ., 2009

76

629.78.018.3:533.6:621.396.67

. . , . . , . .

. . , ,

. . , . .

( ), ,

-

- -

. - 1-. - - -1000 - .

-

() - - - . , () , -, .

, - , - () (). - - . , - s, 0,01, 0,5 2. , .

- - - . - - , - .

- 200 (. 1).

,

, - - .

. 1. :

0; 45

(. 2).

70 q : 1 2. 1 - -

77

. 2 - - - , -.

-70

1

2

qq

. 2.

- , , - - , - , - -1000, - . . . - - TurboDESIGN 7.0 ( ), - - - 1-.

V. . Smirnov, I. A. Maximov, S. G. Kochura


A. B. Nadiradze, V. V. Shaposhnikov

Moscow Aviation Institute (State Technical University), Russia, Moscow

INDICATRIX ACCOUNT OF MATERIALS DISPERSION AT THE ESTIMATIONS OF EROSION-CONTAMINATING PLASMA INFLUENCE OF THE STATIONARY PLASMA

THRUSTERS ON THE SPACE CRAFT STRUCTURE ELEMENTS The approach to estimate accuracy increase of the erosion-contamination plasma influence of the stationary

plasma thrusters on the space craft structure elements by means of indicatrix account of materials dispersion is investigated in the report. The experiment on the dispersion indicatrix definition of one of the constructional ma-terial L1-P ribbon is described in the article. The results of the comparative analyses of the radiator contami-nation predicted levels of the Thermal Control System of the perspective unified Express-1000 satellite platform with account and without account of the dispersion indicatrix are presented in the report.

. ., . ., . ., . ., . ., 2009

78

621.396.67

. . , . . , . . , . .

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,

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() :

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79

3. 2 : , - .

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5. . .

- - .

:

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, .

6. - .

7. ( - ).

- , , .

, - . - , , , - , .

f(x, u, z) - x z -

u . y . ,

( ( , , )),y f x u z= Y

- .

v , . . fv(x, u, z) - .

-

min { [ ( ( , , )) ]}M W f x u z yY * (1)

,u u W z = z,

M ; W[ ] y y* ( , W ); z ; u -.

- (1) , .

- - -. - - - u. - .

, , 2:

( , , , , 1, ),i i i iV W v z u i n= =

Wi - zi vi -; ui , - .

uj, j = 1, m (m u) -

( , , ),uj j W v z= j j = 1, m. (2)

, uj, j = 1, m , (2) .

(2) - .

80

N. A. Testoyedov, V. V. Dvirnyi, V. I. Khalimanovich, G. V. Dvirnyi


L. V. Dolgov

FSUE Design Engineering Bureau Arsenal named after M. V. Frunze, Russia, Saint Petersburg

CONCEPTION OF THE LARGE SIZED TRANSFORMED STRUCTURES FOR THE SPACECRAFT

Large sized transformed multifunction structure conception which provides the maximum possible rocking an-

gles is proposed in the report.

. ., . ., . ., . ., . ., 2009

621.372.83.001.24

. . , . . , . . , . .

. . , ,

. . , . .

, ,

-

- -

, - .

, --

() - , - .

, - . - - - , .

- , - -, , - , - .

, , , -

, , , . () - , - ( -) , , - .

- , , . . , - - -.

- -, . , - - -

81

, . -: , - , . .

, , - -, - -, , , . , - , , - -.

- . - () - -, , -, -.

, - - , .

-

, - , , - - .

- , , - , , -, - - , , - , - .

- , , -- .

- - , - . - - .

, .

- - - - .

N. A. Testoedov, V. I. Khalimanovich, M. M. Mihnev, V. Yu. Gusev


P. N. Silchenko, I. V. Kudryavcev


PROVIDING THE ENGINEERING SOLUTIONS AT DESIGNING OF SOLDERED WAVEGUIDE DISTRIBUTIVE SYSTEMS OF SPACE COMMUNICATION SATELLITES

Proposals of calculation methods of stress analysis of straight and curved elements with thin-walled sections

as well as soldered joints between them by means of couplings and flanges to produce waveguide distributive sys-tem are considered.

. ., . ., . ., . ., . ., . ., 2009

82

621.372.83.001.24

. . , . . , . . , . .

. . , ,

. . , . . , . .

, ,

-

--

() .

, , , , - - . - - - - .

- -, , . , - - . - - . - () . - - -. - - - , . , .

, - , , ,

- - - -- .

- , -, - , - -, --. - 115,5; 136,5; 3515; 6110; 5825 ( - 205133293 28. 10. 05 - ).

- - , - , - - - , . - - 1540 - .

- - , - , - -- - .

-- -

83

, , -, 20 % -, 1520 % , 2...2,5 , - .

- - . . - .

N. A. Testoedov, V. I. Khalimanovich, M. M. Mihnev, V. Yu. Gusev


P. N. Silchenko, I. V. Kudryavcev, V. I. Ivanov


PROVIDING THE TECHNOLOGY OF PRODUCTION OF SOLDERED WAVEGUIDE DISTRIBUTIVE SYSTEMS OF SPACE COMMUNICATION SATELLITES

The technology of production of separate elements waveguide distributive systems of space communication

satellites with all-round automation of all conditions to excluding the human element is presented.

. ., . ., . ., . ., . ., . ., . ., 2009

621.396.67

. . , . . , . . , . . , . . , . . , . . , . .

. . , ,

. . , . .

, , -

,

-

. - ()

, , , .

- , , - - - .

, , 1000 TELEKM-3, -300, - -, . .

( ) . - - -2009. - - .

- 43 - . --2, - .

- - . . - - .

, - , -

84

- () - (), , -, , - .

, , - , - . , - - -. , , - , -

. - () - - , .

(. ).

54 .

- , - . - .

N. A. Testoedov, V. E. Kosenko, V. V. Dvirnyi, R. P. Turkenich, V. A. Bartenev, D. A. Matronitskiy, G. V. Dvirnyi, G. I. Ovechkin


L. V. Dolgov, V. V. Golovanova

JSC Machine-building plant Arsenal, Russia, Saint Petersburg

PRINCIPLE OF CONSTRUCTION OF TRANSFORMED DESIGNS COMMUNICATION, NAVIGATION AND A GEODESY SATELLITES

In article the new perspective principle of construction of transformed mechanical systems of space vehicles is

offered.

. ., . ., . ., . ., . ., . ., . ., . ., . ., . ., 2009

85

629.78.08.018:629.78.086

. . , . .

. . , ,

-

-

, , - .

(), -

(), () - .

- - .

, - , .

, - , . ( ) - SESAT, , -, - () .

- () . , , . - - .

:

() (-): ;

- ();

; -

() ;

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, , - ;

- (-9);

- .

- (++, Delphi) ActiveX -. ActiveX , - , -.

(. ). , - .

86

Microsoft Excel. : - , - .

- , - , , .

- , - , , - .

- - , - .

E. R. Travyanko, V. V. Smirnov


AUTOMATION OF GROUND EXPERIMENTAL IMPROVEMENT OF WORKING MEDIUM SUBMISSION BLOCKS OF CORRECTION AND ORIENTATION SYSTEMS BY CREATING

THE CONTROL-VERIFYING EQUIPMENT COMPLEX

The control-verifying equipment for the automated tests working medium submission blocks and its elements during their manufacture, computer-controlled by elements and control of functioning on pressure detectors, pressure gauges and temperature gauges, is developed.

. ., . ., 2009

629.78.01

. . , . . , . .

. . , ,

, . - .

- , , - - , -, - .

- , - . -, , (-

- ), - - . , , , , -.

() - - -. - 50 -, . 240 - .

87

- () - , - : . - , (. ). - - - (, - ).

- - , - - . , - , , [1].

- -, 30 %

. -, -, - - . 80 % , , - -, . 60 % , - , -, . , , , . - , .

- - .

- - :

;

;

.

-4

88

, , - . -, :

: -

;

, .

1. , . . - / . . - ; . . ., 2004.

R. P. Turkenich, V. V. Dvirnyi, A. V. Mashukov


FORECASTING THE DATAWARE OF SPACE VEHICLE DESIGNING PROCESSES UNDER THE UNCERTAINTY CONDITIONS

The expert estimation method of database perfection to design complex information systems, such as space ve-

hicles, is a basis for forecasting and an estimating the possibility of innovations. It essentially reduces risks and uncertainty of administrative decision acceptance.

. ., . ., . ., 2009

539.3

. . , . .

. . , ,

C. . , . . , . . , . . , . .

- , ,

,

.

-, [1]. , -.

- - - [2]. , , - - , .

-- [3].

1. , . . / . . , . . -. . : , 1987.

2. , . . - : . 2350519 . / . . [ .]. . 27.03.2009.

3. . . / . . , . . , . . , . . // : . 2004. 10. . 1018.

89

V. I. Khalimanovich, V. V. Shalkov


S. V. Ponomarev, V. G. Butov, M. S. Buhtyak, V. A. Solonenko, A. A. Yashuk


ISSUES OF MODELLING THE UMBRELLA TRANSFORMED REFLECTOR The issues of modelling the umbrella reflector, based on mechanics of the deformed firm body are consid-

ered.

. ., . ., C. ., . ., . ., . ., . ., 2009

629.78

. . , . .

. . , ,

. -

, - . , , . .

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.

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; -

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;

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; ; -

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1) -;

2) - ;

3) - .

, - .

90

- , - , - , - , .

,

, -, -.

- , - , , - .

D. A. Cherepanov, B. G. Porpylev


ISSUE OF ACTUATOR RELIABILITY ASSURANCE DEPLOYMENT

The issues of actuator reliability deployment and the method to deal with that kind of problem are presented.

. ., . ., 2009

669.713.7

. . , . .

. . , ,

l- -

l- . -, .

,

, - . , -. - - .

, - l- , , .

, l- , -.

, - : , -. , l-

-, - . - , , - .

, l- , , , - [13].

- - .

l- .

(. 1) , -.

l1 l2 . -

91

l1 l2 - .

. 1.

, , - , - . , - :

2 22 .y n x l= - + (1)

l1 - :

2 21 ( ) .l m x y= + D + D (2)

(2) x,

cos .x nD = a (3)

(3) (2), - l1:

( ) ( )2

2 221 2cos cosl m n l n n

= - a + - a .

, - l1() (. 2).

. 2.

,

, , .

1. - / . . , . . -, . . . : , 1999.

2. , . . - / . . . . , . . . . : , 1991.

3. , . . - / . . . ., 1983.

A. V. Chernick, N. A. Smirnov


FLAT MECHANICAL SYSTEM BASED

ON l-COORDINATE DEVICES

Non-traditional high precision manipulators for space industry based at l-coordinate devices are considered. Their advantages to other types of manipulators are described. Also methods of inverse kinematics calculation are described.

. ., . ., 2009

92

629.78:531.395

. .

. . , ,

, -

. .

-

, - () - , , - - . - , - -, - , , . - - , - , , - . , - . , - . - , . - . - , , - . - , - . - - -. -

- , - , -, .

- - . , , - , - , . - () , - - . .

, - - , , , . -. .

, - , . - , - -- -, -. - -.

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93

-, - ( -) . .

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; - - , , -, ; , , , - .

, -,

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,

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, %

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, 0,36 0,565 0,376 4,4 0,33 2,86 3,61 3,13 9,44 1,25 3,05 3,70 3,47 13,77 1,17 7,53 16,6 8,04 6,77 7,9 8,5 17,42 8,28 2,6 8,24

12,31 25,48 11,47 6,82 11,34 16,24 32,1 16,47 1,41 16,5 16,3 32,0 16,34 0,25 16,48

S. A. Churilin

Bauman Moscow State Technical University, Moscow, Russia

FINDING THE DYNAMIC CHARACTERISTICS OF SELF-DEPLOYABLE FRAME ANTENNAE USING THE RESULTS OF ITS FREQUENCY TESTS

This paper describes a mathematical model of self-deployable frame space antennae, providing an opportunity

for swing joints influence on frequencies and mode shapes of natural oscillations. The comparative values of ex-perimental and calculated frequencies of frame antennae natural oscillations are presented.

. ., 2009

669.713.7

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