Responsive Access Small Cargo Affordable Launch (RASCAL ...

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Appendix: Conceptual Design Renderings: 54
Page 1 and 2:
Responsive Access Small Cargo Affor
Page 3 and 4:
List of Figures: Figure 1: Launch C
Page 5 and 6:
Abstract: RASCAL is a Defense Depar
Page 7 and 8:
Introduction: Due to the uncertaint
Page 9 and 10: This stage will then propel the veh
Page 11 and 12: stages which continue on to orbit.
Page 13 and 14: driving constraint) will then be fl
Page 15 and 16: Once the geometry is defined it mus
Page 17 and 18: Coefficient of Drag 0.6 0.5 0.4 0.3
Page 19 and 20: These characteristics were then ana
Page 21 and 22: To analyze the effect of MIPCC an A
Page 23 and 24: 14. The new Isp of the MIPCC engine
Page 25 and 26: combination selected the overall we
Page 27 and 28: Table 5: POST Trajectory Constraint
Page 29 and 30: Thrust (lbs) 120000 100000 80000 60
Page 31 and 32: Gross Gross Weight Dry Dry Weight W
Page 33 and 34: Temperature (F) 1400 1300 1200 1100
Page 35 and 36: Operations: Number 1st Stages 5 Num
Page 37 and 38: Cost Estimation: The cost estimatio
Page 39 and 40: As this figure depicts the DDT&E fo
Page 41 and 42: profile of the cost charts is due t
Page 43 and 44: Each of these alternatives will be
Page 45 and 46: 1+2+3 1+3 4th Stage MMC 1st Lox Hyb
Page 47 and 48: The design alternatives were costed
Page 49 and 50: GT RASCAL: From this alternative an
Page 51 and 52: As this figure shows the GT RASCAL
Page 53 and 54: used in the GT RASCAL design is in
Page 55 and 56: Figure 39: GT RASCAL Mission Profil
Page 57 and 58: When the final cost numbers of the
Page 59: References: 1. Cyr, Kelley, “US L
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