Author:
Zhang Xin-ai,Tang Hai-bin
Reference33 articles.
1. Oleson SR, Myers RM, Kluever CA, Riehl JP, Curran FM (1997) Advance propulsion for geostationary orbit insertion and north-south station keeping. J Spacecr Rocket 34(1):22–28
2. Curran FM, Hagg TW (1992) Extended life and performance test of a low-power arcjet. J Spacecr Rocket 29(4):444–452
3. Lichon PG, Sankovic JM (1996) Development and demonstration of a 600-second mission-average Isp arcjet. J Propuls Power 12(6):1018–1025
4. Smith RD, Yano SE, Armbruster K, Roberts CR, Lichtin DA, Beck JW (1993) Flight qualification of a 1.8 kW hydrazine arcjet system. In: International electric propulsion conference. IEPC-93-007
5. Smith RD, Roberts CR, Aadland RS, Lichtin DA, Davies K.(1997) Flight qualification of the 1.8 kW MR-509 hydrazine arcjet system. In: International electric propulsion conference. IEPC-97-081