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SAE technical paper series, Volume 941326.
A proof-of-concept (POC) lightweight lunar radiator was fabricated and tested. The POC radiator has a specific weight of 5 kg/kW one quarter the specific... 
Nuclear energy | Spacecraft | Thermal management | Radiators
eJournal
SAE technical paper series, Volume 961456.
Current state-of-the-art space radiators are too heavy (5-7 kg/m2) and voluminous to be feasible for some future space missions. Accordingly, there is a need... 
Tests and Testing | Radiators
eJournal
SAE technical paper series, Volume 921023.
This paper presents the design and performance of a flexible heat pipe cold plate (FHPCP) that was developed for transporting heat from electronics mounted... 
Thermal management | Military aircraft | Engine cooling systems
eJournal
SAE technical paper series, Volume 951436.
The current trend in military avionics design is to physically move electronics closer to the components they control. This saves on weight, increases... 
Thermal management | Avionics
eJournal
SAE technical paper series, Volume 961319.
This paper describes the transfer of Russian fine pore sintered powder metal wick structure fabrication technology to the United States for use in the... 
Fabrication
eJournal
SAE, International Conference on Environmental Systems, 28th, Danvers, MA; UNITED STATES; 13-16 July 1998, 07/1998
... of starting flight tests in early 1999. (Author) 
Conference Proceeding
ANS, SAE, AIChE, AIAA, et al., IECEC - Intersociety Energy Conversion Engineering Conference, 33rd, Colorado Springs, CO; UNITED STATES; 2-6 Aug. 1998, 08/1998
... of starting flight tests in early 1999. (Author) 
Conference Proceeding
ANS, SAE, AIChE, AIAA, et al., IECEC - Intersociety Energy Conversion Engineering Conference, 33rd, Colorado Springs, CO; UNITED STATES; 2-6 Aug. 1998, 08/1998
To improve flight control system weight, reliability, maintainability, and supportability, electronic packages that were normally located in the cockpit are... 
Conference Proceeding
SAE, Aerospace Atlantic Conference, Dayton, OH; UNITED STATES; 23-25 May 1995, 05/1995
Moving military electronics closer to the components they control saves on weight, increases component maintainability, reduces aircraft manufacturing costs,... 
Conference Proceeding
ANS, SAE, AIChE, AIAA, et al., IECEC - Intersociety Energy Conversion Engineering Conference, 33rd, Colorado Springs, CO; UNITED STATES; 2-6 Aug. 1998, 08/1998
.... Model accuracy is confirmed by comparison to thermosyphon test data for a variety of working fluids. (Author) 
Conference Proceeding
ANS, SAE, AIChE, AIAA, et al., IECEC - Intersociety Energy Conversion Engineering Conference, 33rd, Colorado Springs, CO; UNITED STATES; 2-6 Aug. 1998, 08/1998
A unique thermosyphon condenser design is presented that utilizes drainage disks in the condenser to reduce the liquid film thickness and consequently the... 
Conference Proceeding
Space Technology and Applications International Forum (STAIF-96); Proceedings of the 1st Conference on Next Generation Launch Systems and 2nd Spacecraft Thermal Control Symposium, Albuquerque, NM, Pt. 2; UNITED STATES; 7-11 Jan. 1996, 01/1996, pp. 721 - 729
This paper describes the design and testing of a Loop Heat Pipe Radiator (LHPR) which was developed as an alternative to state-of-the-art axially grooved heat... 
Conference Proceeding
SAE, International Conference on Environmental Systems, 28th, Danvers, MA; UNITED STATES; 13-16 July 1998, 07/1998
A planetary outpost flexible heat pipe heat rejection radiator was designed-to reject 25 kW of waste heat. To confirm its performance, a representative segment... 
Conference Proceeding
SAE 1994 Transactions, Journal of Aerospace. Section 1 - Vol. 103 (A96-37718 10-31); UNITED STATES, 01/1995, pp. 689 - 698
A proof-of-concept (POC) lightweight lunar radiator was fabricated and tested. The POC radiator has a specific weight of 5 kg/kW one quarter the specific... 
Conference Proceeding
IN:SAE 1994 Transactions, Journal of Aerospace. Section 1 - Vol. 103 (A96-37718 10-31), Warrendale, PA, Society for Automotive Engineers, Inc., 1995, p. 689-698, 01/1995
A proof-of-concept (POC) lightweight lunar radiator was fabricated and tested. The POC radiator has a specific weight of 5 kg/kW one quarter the specific... 
Conference Proceeding
AIAA, Aerospace Sciences Meeting & Exhibit, 36th, Reno, NV; UNITED STATES; 12-15 Jan. 1998, ISSN 0146-3705, 01/1998
.... This paper reports the results of testing these LHPs. (Author) 
Conference Proceeding
Space nuclear power and propulsion; Proceedings of the 10th Symposium, Albuquerque, NM, Pt. 1; UNITED STATES; 10-14 Jan. 1993, 01/1993, pp. 395 - 405
A proof-of-concept (POC) ultralightweight lunar radiator was fabricated and tested. The POC radiator has a specific weight of 5 kg/kW, which is one-quarter the... 
Conference Proceeding
Space Technology and Applications International Forum (STAIF-96); Proceedings of the 1st Conference on Next Generation Launch Systems and 2nd Spacecraft Thermal Control Symposium, Albuquerque, NM, Pt. 2; UNITED STATES; 7-11 Jan. 1996, 01/1996, pp. 753 - 763
Organic matrix composite material is recognized for its significant strength to weight ratio when compared to metal and consequently was investigated for... 
Conference Proceeding
Space Technology and Applications International Forum (STAIF-96); Proceedings of the 1st Conference on Next Generation Launch Systems and 2nd Spacecraft Thermal Control Symposium, Albuquerque, NM; UNITED STATES; 7-11 Jan. 1996, 01/1996, pp. 889 - 894
This paper describes the development of lightweight aluminum foil lined polymer matrix composite tubing for applications ranging from heat pipe construction to... 
Conference Proceeding
RSC advances, ISSN 2046-2069, 2016, Volume 6, Issue 75, pp. 71557 - 71566
...-Scherer, c U. Gernert, d J. P. Rabe, c J. Kneipp * a and E. Kemnitz * a Porous MgF 2 -over-nanoparticles (MON) surfaces are fabricated from immobilized gold... 
Journal Article
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