Buran/Energia drawings

The scale of the drawings is 1/200 although it might differ if you 
print-to-fit. The numbers listed are for 1/1 scale in milimeters

Translations of the images:
- part3a
  Pogled =look, obrnjeno = reverse, povecano = enlarged.
- part1bc
  Raketno-vesoljski kompleks Energija-Buran
  Rocket space complex Energia-Buran
  Vir - Source
- part 2b, part 3b, Parts list only:
  Nosilna raketa energija - Energija carrier rocket
	1-Oxygene tank block C
	2-midsection between tanks
	3-upper link-connector between blocks A and C
	4-Hydrogene tank block C
	5-pressurised pipelines of oxygene tank
	6-telemetric system antennas
	7-hydraulics pannel
	8-Buran holder
	9-tail section of block C
	10-lower link between A and C blocks
	11-solid rocket boosters to separate stages
	12-hydrogen pipelines
	13-first stage engines cover
	14-pressurised hydrogen pipelines
	15-cable cover of block C
	16,17-covers for parachute systems of block A
	18-lower Buran holder
	19-Buran holder&cable connection
	20-upper links between A blocks (parablock)
	21-lower links between A blocks (parablock)
	22-pneumatohydraulics switches of block C
	23-oxygene tank of block A
	24-kerosine tank of block A
	25-separation boosters for blocks A (parablock)
	Pictures A and D are showing ties between A blocks (parablock) M1-M4
  Buran cosmoplan:
	1-nose guiding engines
	2-main entry hatch
	3-pressurising carriage section holes
	4-cargo bay doors
	5-tail, aerodynamic brake
	6-parachute braking system
	7-joint engine modul (ODU)
	8-moving protector-rudder
	9-orbital manuevering exaust
	10-illuminator window
	11-tail section guiding engines
	12-elevons
- part 2c:
  Shema barvanja - paint sheme
  colours from top to bottom:
	white
	light grey
	grey
	metal - steel
	red
	brown
	black

- part 2b: Translation of technical data

Technical data of Energia/Buran complex (extraction from data revieled at 
38th international air show Le Bourget, year 1989):

Total mass before lift off		max 2400 t

ENERGIA launch vehicle:
Joint engines thrust power
1st and 2nd stage			35.50 MN
Lift off G				1.48 G
RD-170 liquid fuel engine thrust:
- at sea level				7.4 MN
- in vacuum				8.06 MN
2nd stage liquid fuel engine:
- at sea level				1.480 MN
- in vacuum				2 MN
Mass of Energia without fuel 
(construction only)			approx. 300 t

BURAN orbiter:
Lift off mass				105 t
Landing mass				max 82 t
Mass of the construction		62 t
Usefull cargo mass:
- in 250 km orbit			max 30 t
- in 450 km orbit			max 27 t
Mass of returning cargo			max 20 t
ODU fuel mass:
- default				8 t
- max					14 t
Highest orbit (max ODU)			800 - 1000 km
Liquid fuel engines trust		2 x 88 kN
Number and steering liquid 		38 x 3870 N
fuel engines (RSU)			and 8 x 200 N
Wing area				250 m^2
Crew cabin volume			73 m^3
Landing speed				340 km/h

These drawings were published in TIM magazine, issue Speptember 1998, article by Vojko Kogej.
Original drawings were printed on A2 format. The source for the plans is 
listed in the bottom of plan1bc.jpg.
There may be still some issues left. To get your own copy of the magazine 
contact Joze.Cuden@guest.arnes.si.
TIM is published by Tehniska Zalozba Slovenije.
http://www.tehniska-zalozba.si