Rocketdyne (5228 bytes)
3: ...bought by Boeing in December, [[1996]]. As such, Rocketdyne is currently a part of [[Boeing Integrated Defens...
5: ...e. As the missile entered production NAA spun off Rocketdyne in 1955 as a separate division.
7: Rocketdyne's next major development was their first all-new ...
9: ...(soon to become [[Rockwell International]]), with Rocketdyne as a major division.
11: ...t]] division in 1983. The rest of NAA, along with Rocketdyne, was sold to Boeing in 1996.

Rocketdyne Santa Susana Field Laboratory Contamination (18417 bytes)
4: ... workers, and nearby residents near [[Boeing]]'s (Rocketdyne's) rocket and nuclear test facility known as the ...
12: ...ensus Tract Cancer Data of the deceased workers. Rocketdyne workers who are ''living with cancer'' are ''not'...
14: [[image:Rockreactor.jpg]]<br><font size="2">Rocketdyne Nuclear Sodium Reactor Experiment: Containment Bu...
16: ...p://www.geocities.com/madelinefelkins/911rock.htm Rocketdyne Worker Health Study]. Also, the study reports the...
22: ...e [http://www.ph.ucla.edu/erg/meeting_slides.html Rocketdyne Community Resident Health Study], which examines ...

RD (71 bytes)
2: * [[Rocketdyne]]

F-1 (rocket engine) (3909 bytes)
4: ...ed by an engine with so much power and contracted Rocketdyne to complete the development of the F-1. The firs...
23: <br>Contractor: NAA/Rocketdyne
27: ...n uprating redevelopment of the F-1 undertaken by Rocketdyne during the 1960s which resulted in a new engine s...

Delta II/III Launch Vehicle Family (411 bytes)
1: .../III Launch Vehicle Family''' was developed by [[Rocketdyne]]/[[Boeing]] at Chatsworth and Canoga Park, Calif...

RS-68 (rocket engine) (2056 bytes)
5: It was developed at [[Rocketdyne]] Propulsion and Power, located in Canoga Park, C...
14: ...w.boeing.com/defense-space/space/propul/RS68.html Rocketdyne's RS-68 page.]

F-1 (rocket engine)/Temp (699 bytes)
19: <br>Contractor: NAA/Rocketdyne

Poseidon class Supercarrier (2643 bytes)
7: ...estroyer]]. Many of the design principles used by Rocketdyne are shared between the Poseidon, the Omega and th...

Convair X-11 (1089 bytes)
10: *'''Powerplant:'''Two [[Rocketdyne XLR-89-1]] rocket motors burning [[Liquid oxygen|...

J-2 (rocket engine) (1118 bytes)
15: <br>Contractor: NAA/Rocketdyne

Boeing X-37 (3636 bytes)
5: ...n advanced airframe. The on-board engine is the [[Rocketdyne]] AR-2/3, which is fueled by [[Hydrogen Peroxide]...
25: ...' initially none, follow up vehicle may have 1x [[Rocketdyne AR2-3]], 29.3 kN (6,582 lb) thrust (vacuum)

Turbopump (1458 bytes)
13: ...bopumps for Liquid Rocket Engines] &ndash; From [[Rocketdyne]]'s ''Engineering Journal of Power Technology''

Saturn (rocket family) (5984 bytes)
9: ...on [[Thor (rocket)|Thor]] and Jupiter missiles. [[Rocketdyne]], the manufacturer of the S-3D received a contra...
11: At the same time, Rocketdyne designed a single engine that would meet the requ...
31: ...ent of a new hydrogen-burning engine was given to Rocketdyne in [[1960]] and for the development of the Saturn...

Rockwell (3689 bytes)
5: ...vstar [[Global Positioning System]] satellites. [[Rocketdyne]], who had been spun off by North American in 195...
13: ...[Boeing Integrated Defense Systems]], including [[Rocketdyne]] in December, 1996. The company began to spin of...

Canoga Park, Los Angeles, California (1552 bytes)
5: In [[1955]] the [[Rocketdyne]], then a spinoff of [[North American Aviation]],...

North American Aviation (4525 bytes)
16: ...ngine division spun off into a separate company [[Rocketdyne]] in [[1955]], but North American designed and bu...
20: ...tional (including the North American Aviation and Rocketdyne divisions) merged with [[Boeing]].

H-1 (rocket engine) (2511 bytes)
63: * Contractor: NAA/Rocketdyne

Atlas II (5246 bytes)
94: **Principal subcontractors: Rocketdyne (Atlas engine, MA-5); Pratt & Whitney (Centaur en...
95: **Power Plant: Three MA-5A Rocketdyne engines, two Pratt & Whitney RL10A-4 Centaur engi...

Delta II rocket (2284 bytes)
13: *Stage I: Fuel and oxygen tanks that feed the [[Rocketdyne]] main engine for the ascent.

AGM-53 Condor (2293 bytes)
20: *Propulsion: Rocketdyne MK 70 solid-fueled rocket motor

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