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The Falcon Launch Vehicle:

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Title: The Falcon Launch Vehicle:


1
The Falcon Launch Vehicle Towards Operationally
Responsive Space
Space Exploration Technologies 1310 Grand
Avenue El Segundo, CA 90245 Phone (310) 414-6555
X 228 Fax (310) 414-6552 spacex.com
The views, opinions and/or findings contained in
this article are those of the author and should
not be interpreted as representing the official
policies, either expressed or implied of the
Defense Advanced Research Projects Agency or the
Department of Defense
2
Background and Programmatic Progress
  • SpaceX, under private investment, is developing a
    reliable, low cost launch vehicle in the light
    payload class
  • As a result of the relatively simple design,
    robust margins, and the necessity to keep prices
    low, Falcon is a responsive launcher
  • Programmatic Progress
  • SpaceX has developed the facilities, holds all
    permits and licenses, and has developed the
    documentation necessary to build, test, and
    transport Falcon to VAFB
  • State Department, 8 separate Environmental
    regulatory agencies, the ATF, the Western Test
    range and our local Fire Departments
  • Agreement in place with the Army to operate from
    Kwaj
  • Business Progress
  • First launch contracted with support from the
    Secretary of Defense
  • Government Mission assurance review initiated
  • First customer signed for the Falcon V

3
Falcon SLV Technical Status
  • Kestrel development nearly complete robust c
    efficiency indicating a 327 Isp (which exceeds
    goal)
  • Merlin component development complete full
    engine development near complete
  • Structural qualification begun
  • Flight tankage in manufacture
  • Complete prototype vehicle integrated as a
    manufacturing pathfinder
  • Range telemetry successfully completed
  • Command and Control Van and transporter erector
    nearly complete

4
November 2003
Proto-Falcon final assembly on the precision
manufacturing track
5
Falcon in Washington DC for its Unveiling
6
Technical Summary-- Falcon SLV
  • Payload capability Over 1500 lbs to LEO (28.5
    deg, 100 nm, circular)
  • Launch from Vandenberg, Kwajelein, and the Cape
  • Multiple manifest, multiple orbit
  • Very benign payload environment
  • 5.9M per launch plus range fees for single
    flight contracts
  • Vehicle flight ready by mid 2004
  • Diameter 5.5 tapering to 5
  • Length 68
  • 1st Stage Parachute/Water Recovery
  • 1st Stage Lox/RP1
  • 2nd Stage Lox/RP1

7
Falcon First Stage
  • Re-usable 1st Stage
  • Lox RP1 Propellant
  • Aluminum 2219-T6 Tanks
  • Flight Pressure Stabilized Design
  • Common bulkhead
  • 94 Mass Ratio
  • Parachute to Water Landing
  • SpaceX Merlin Engine
  • Thrust 72k SL, 85k Vacuum
  • Isp 261 SL, 310 Vacuum
  • Ablatively Cooled
  • Pintle Injector Geometry
  • Pump-fed Gas Generator Cycle
  • Turbine Exhaust Roll Control
  • Hydraulic TVC

8
Merlin Engine Test
9
Falcon Second Stage
  • Expendable 2nd Stage
  • Lox RP1 Propellant
  • Aluminum Lithium Tanks
  • Common Bulkhead
  • 91 Mass Ratio
  • Engine
  • 7.5Klbf Vacuum Thrust
  • Pressure Fed with GHe
  • Isp 325 Vacuum
  • Hot Helium Attitude Control
  • Ablative/Radiative Cooling
  • Pintle Injector Geometry
  • EMA for TVC

10
Kestrel Engine Test
11
Falcon Performance from VAFB
12
Performance from VAFB Varying Inclination
13
Performance From Kwajalein
14
Predicted Injection Accuracies
Predicted accuracies
  • Published accuracies
  • inclination /- 0.1 deg
  • perigee /- 10 km
  • apogee /- 20 km

15
Launch Sites Falcon I and Falcon V
  • SLC 3W at the Western range (VAFB) for high
    inclination launches
  • Reagan Test Site (Kwaj) for low to mid
    inclination launches
  • Agreements also in place for LC-46 at the Eastern
    Range

16
Transporter/Erector
17
Launch Timeline, Standard SLV Mission
18
Falcon Launch Operations
19
Hurdles The Non-Responsive Part
  • Operationally responsive space requires extensive
    non-recurring/preparatory effort (i.e. not
    responsive)
  • Hurdles are developmental and regulatory in
    nature
  • Development hurdles include the capital
    investment and technical development leading to
    production of a low cost capability
  • Regulatory elements include
  • MOA for launching Annexes for individual Federal
    Sites
  • Environmental? FONSI
  • Environmental permits
  • Site license
  • Range Safety Approval
  • (FAA License)
  • ATF
  • DOT
  • SpaceX has been successful in clearing the
    hurdles and is looking forward to first flight
    this summer
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