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Search
A p p e a r a n c e
● C r e a t e a c c o u n t
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P a g e s f o r l o g g e d o u t e d i t o r s l e a r n m o r e
● C o n t r i b u t i o n s
● T a l k
( T o p )
1
C o n f i g u r a t i o n
2
C h a r a c t e r i s t i c s
3
E x t e r n a l l i n k s
4
R e f e r e n c e s
T o g g l e t h e t a b l e o f c o n t e n t s
L K - 1
2 l a n g u a g e s
● F r a n ç a i s
● Р у с с к и й
E d i t l i n k s
● A r t i c l e
● T a l k
E n g l i s h
● R e a d
● E d i t
● V i e w h i s t o r y
T o o l s
T o o l s
A c t i o n s
● R e a d
● E d i t
● V i e w h i s t o r y
G e n e r a l
● W h a t l i n k s h e r e
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● U p l o a d f i l e
● S p e c i a l p a g e s
● P e r m a n e n t l i n k
● P a g e i n f o r m a t i o n
● C i t e t h i s p a g e
● G e t s h o r t e n e d U R L
● D o w n l o a d Q R c o d e
● W i k i d a t a i t e m
P r i n t / e x p o r t
● D o w n l o a d a s P D F
A p p e a r a n c e
F r o m W i k i p e d i a , t h e f r e e e n c y c l o p e d i a
T h e p r i n t a b l e v e r s i o n i s n o l o n g e r s u p p o r t e d a n d m a y h a v e r e n d e r i n g e r r o r s . P l e a s e u p d a t e y o u r b r o w s e r b o o k m a r k s a n d p l e a s e u s e t h e d e f a u l t b r o w s e r p r i n t f u n c t i o n i n s t e a d .
The LK-1 had its origin in several early 1960s spacecraft projects under the generic names of kosmoplans and raketoplans .[2]
In 1965 the project was cancelled in favour of the Soyuz 7K-L1 spacecraft.[2]
Further developments came as the LK-700 direct-descent lunar lander program.
Configuration
An drawing of a VA spacecraft : The VA capsule is on the lower right, while the braking engines are located on top of the long "nose section".[3] [4] The launch escape system (not shown) would have been attached on top of the nose section.[5]
The spacecraft consisted of the following modules:
ADU Emergency Engine Unit
VA Capsule (crew module)
PAB Equipment-Rocket System Block (service module)
RB Translunar Injection Stage
Characteristics
Crew Size: 2
Spacecraft delta v: 3,300 m/s
Electric System: 2.00 average kW.
Gross mass: 17,000 kg
Un-fuelled mass: 4,000 kg
Height: 5.20 m
Span: 7.27 m
External links
References
^ "TKS transport ship 11F72" . RussianSpaceWeb.com. Archived from the original on 17 August 2012. Retrieved 30 August 2012 .
^ "TKS-VA (11F74)" . Gunter's Space Page. Retrieved 1 September 2012 .
^ "TKS" . Encyclopedia Astronautica . Archived from the original on 25 August 2012. Retrieved 31 August 2012 .
t
e
Active
In development
Past
Cancelled
Moon: Zond (7K-L1) , N1-L3 , LK-700 , Zvezda
Interplanetary: TMK , Aelita , Martian Piloted Complex
Spaceplanes: Spiral , Energia / Buran , MAKS , Kliper , LKS , Tupolev Tu-2000
Capsules: Zvezda , Zarya
Space Stations: OPSEK
Related
t
e
Crewed lunar spacecraft
Orbiters
Landers
Proposed
Related
R e t r i e v e d f r o m " https://en.wikipedia.org/w/index.php?title=LK-1&oldid=1084407485 "
C a t e g o r i e s :
● C r e w e d s p a c e c r a f t
● C a n c e l l e d S o v i e t s p a c e c r a f t
● S o v i e t l u n a r p r o g r a m
● C r e w e d s p a c e p r o g r a m o f t h e S o v i e t U n i o n
● N P O M a s h i n o s t r o y e n i y a p r o d u c t s
● T h i s p a g e w a s l a s t e d i t e d o n 2 4 A p r i l 2 0 2 2 , a t 0 8 : 5 3 ( U T C ) .
● T e x t i s a v a i l a b l e u n d e r t h e C r e a t i v e C o m m o n s A t t r i b u t i o n - S h a r e A l i k e L i c e n s e 4 . 0 ;
a d d i t i o n a l t e r m s m a y a p p l y . B y u s i n g t h i s s i t e , y o u a g r e e t o t h e T e r m s o f U s e a n d P r i v a c y P o l i c y . W i k i p e d i a ® i s a r e g i s t e r e d t r a d e m a r k o f t h e W i k i m e d i a F o u n d a t i o n , I n c . , a n o n - p r o f i t o r g a n i z a t i o n .
● P r i v a c y p o l i c y
● A b o u t W i k i p e d i a
● D i s c l a i m e r s
● C o n t a c t W i k i p e d i a
● C o d e o f C o n d u c t
● D e v e l o p e r s
● S t a t i s t i c s
● C o o k i e s t a t e m e n t
● M o b i l e v i e w