Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

---

XLR13-AJ-7

---

AKA: X60ALD-4000. Date: 1948. Thrust: 17.60 kN (3,957 lbf). Burn time: 60 s. Height: 3.43 m (11.25 ft). Diameter: 0.81 m (2.65 ft).

Thrust (sl): 17.600 kN (3,957 lbf). Thrust (sl): 1,800 kgf. Engine: 363 kg (800 lb). Chamber Pressure: 21.00 bar. Propellant Formulation: RFNA/80% Aniline+20%Furfuryl alcohol.