8
10 ROCKET SYSTEMS TEST SITES In this area, hydrogen-oxygen rocket engines are fired and data is obtained on heat transfer between the hot gases and the nozzle walls. Also, studies are made on heat transfer from the nozzle wall to the liquid hydrogen used to cool the nozzle. This heat transfer research is being done to support the development of nozzles for nuclear rocket engines. Also located in this area is a space environment tank, where various types of liquid hydrogen propellant tanks can be tested at space conditions. Various types of tank insulations are being studied. The 38-foot diameter steel hydraul ics laboratory used liquid oxygen under pressures inch. containment vessel is a to test liquid fluorine and up to 1200 pounds per square CONTROL AREA

ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,

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Page 1: ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,

10

ROCKET SYSTEMS TEST SITES

In this area, hydrogen-oxygen rocket engines are firedand data is obtained on heat transfer between the hotgases and the nozzle walls. Also, studies are made onheat transfer from the nozzle wall to the liquid hydrogenused to cool the nozzle. This heat transfer research isbeing done to support the development of nozzles fornuclear rocket engines.

Also located in this area is a space environment tank,where various types of liquid hydrogen propellant tankscan be tested at space conditions. Various types oftank insulations are being studied.

The 38-foot diameter steelhydraul ics laboratory usedliquid oxygen under pressuresinch.

containment vessel is ato test liquid fluorine andup to 1200 pounds per square

CONTROL AREA

Page 2: ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,

10 ROCKET SYSTEMS TEST SITES

In this area, hydrogen-oxygen rocket engines are firedand data is obtained on heat transfer between thehot exhaust gases and the nozzle walls. Studies arealso mode on heat transfer from the nozzle wallto the liquid hydrogen used to cool the nozzle. Thisheat transfer research is being done to support thedevelopment of nozzles for nuclear rocket engines.

Also located in this area is a space environment tankwhere different types of liquid hydrogen propellanttanks can be tested at space conditions. Varioustypes of tank insulations are being studied.

The 38' diameter steel containment vessel is a hy-

draulics laboratory used to test liquid fluorine andliquid oxygen under pressures up to 1200 poundsper square inch.

Page 3: ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,
Page 4: ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,

JANUARY. 1969 NASA LEWIS RESEARCH CENTER - PLUM BROOK STATION

SANDUSKY. OIUO

4.1517iI

12 1 W X 12'H OPG,

5 'W X 12 'H OPG,

../"- .......\

i \

I LHZ TANK :

\"~

J-J TEST CELLAREA 101

FIRST FLOORREF. DRWG, PF-20946

J SITE Jl AND J3 TEST BUILDINGBUILDING NO.

2711

8 01 __

SCALE 1/16"

16.l' -0"

Page 5: ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,

4.162Til

8 01_ •SCALE 1/16"

16,

l' -0"

CAPS,AND

NASA LE\HS RESEARCH CENTER - PLUM BROOK STATION

SANDUSKY, OH IO

" "';"

.....:.>

UPPERJ-l TEST Cell

5'W X 11'H OPG,-t -L5 ,w x 11'H OPG,

J:"-=~=i=~~~".;;JL1S'w x 12'H OPG,

SeCOND FLOORREF, DRWG, PF-10946

J SITE Jl AND J3 TEST BUILDINGBUilDING NO.

2711

JANUARY. 1969

Page 6: ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,

JANUARY, 1969 NASA lEliIS RESEARCH CENTER - PlUI'I BROOK STATIONSANDUSKY. OHIO

4.172713 & 2714

.~\, >:f.'

'.: .... :

____LEARTH MO~ND

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

I

L__i

2713

J SITE J5 TEST BUILDINGREF. DRWG, PD-21575

2714

J SITE J5 CONTROL TANKREF, DRWG. PF-22567

J SITE JS TEST BUILDING AND JS CONTROL TANKSTRUCTURE NOS,

2713 & 2714 SCALE

• 16, ,

1/16" " 1'-0"

Page 7: ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,

4.182721, 2731 & 2732

NASA lEWIS RESEARCH CENTER - PLUM BROOK STATION

SANDUSKY, OHIO

JANUARY, 1969

o

SAFETY SHOWERROOM 104

LOCKER ROOM I103

250 SF1712 SF

SHOP AREA101-102

10'-0"W X 8'-0"H OPG,

OFFICE105

120 SF

OFF I CE106

153 SF

12'-0"W X 11 '-6"H OPG,

r-HOOK HT, 13'CAP, 1 TON

II

LCRANE RAIL 13'I NO HOOK

II

-JTt-0 5F 29 SF

HOT WATER SAFETY SHOWERTANK ROOM 101 __ ROOM 102

- --

2721

J SITE SHOPREF, ORWG, PF-20942

174 SF

~d= d

,-"v2731

J SITE SAFETY SHOWER BU IL] INGREF, DRWG, PF-SK-670908C

I~

2732

J SITE BOllER HOUSEREF, DRWG, PF-22584

I

I

~J SITE SHOP, SAFETY SHOWER BUILDING AND BOILER HOUSE

e 0I •SCALE

8 16, ,

1/16' • 1'-0"

8UILOING NOS,

2721 & 2731

STRUCTURE NO,

2732

Page 8: ROCKET SYSTEMS TEST SITES - NASA · J Site Description and floor plans Subject: J Site Description and floor plans Keywords: J Site, Rocket Systems Test Site , Rocket Systems Area,

JANUARY, 1969

LOCATI ON OF WINDOWSVARY WITH CAMERASTAND LOCATION

NASA lElIIS RESEARCH CENTER - PlUIl BROOK STATIlIlSANDUSKY. OHIO

,--------i---J2791

J SITE CAMERA STANDS(1. 2 & 31

REF. DRWG, PF-S~-670909

4.192791 & 2792

~ ~

c-----'-------- '-------

OBSERVATION ROOM 101

214 SF

F--------'~ ~

I-

J SITE CAMERA STANDS (1, 2 &3) AND OBSERVATION TANKSTRUCTURE NOS.

2791 & 2792

l - EARTH MOUND

2792

J SITE OBSERVATION TANKREf, DRWG, Pf-SK-670903D

4 01_ ....SCALE

4 8, ,

1/8" l' -0'