Editing Deep Space 1 (section)

==Statistics==
* Launch mass: {{convert|1071|lb|kg|order=flip|abbr=on}}
* Dry mass: {{convert|822|lb|kg|order=flip|abbr=on}}
* Fuel: {{convert|68|lb|kg|order=flip|abbr=on}} of [[hydrazine]] for attitude control thrusters; {{convert|181|lb|kg|order=flip|abbr=on}} of [[xenon]] for the NSTAR ion engine<ref name="flyby.press.kit" />
* Power: 2,500 watts, of which 2,100 watts powers the ion engine
* Prime contractor: [[Spectrum Astro]], later acquired by [[General Dynamics]], and later sold to [[Orbital Sciences Corporation]]
* Launch vehicle: Boeing [[Delta II]] 7326
* Launch site: [[Cape Canaveral Air Force Station]] [[Cape Canaveral Air Force Station Space Launch Complex 17|Space Launch Complex 17A]]
* Total cost: {{US$|149.7 million}}
* Development cost: {{US$|94.8 million}}
* Personnel:
** Project manager: David Lehman
** Mission manager: Philip Varghese
** Chief mission engineer and deputy mission manager: Marc Rayman
** Project scientist: Robert Nelson